ARCHETYPE: Projectile on an Incline

Watch a ski jumper land. She flies off the ramp at over 90 km/h, arcs through thirty metres of air — and touches down so gently her knees barely flex. The secret is not the snow: it is the hill. Landing slopes are built at close to the flight path's own angle, so the jumper's parabola and the ground meet almost tangentially. Whoever designed that hill was solving, professionally, the exact problem this article drills: a projectile launched over ground that is itself tilted. Examiners love this setup for a precise reason. Ordinary projectile motion hands you a horizontal floor for free — launch and landing levels agree, and the famous formulas R=u2sin⁡2α/gR = u^2\sin 2\alpha/g and T=2usin⁡α/gT = 2u\sin\alpha/g do all the work. Tilt the floor by an angle β\beta and every one of those formulas silently dies. Students who memorised results reach for sin⁡2α\sin 2\alpha and lose the question in the first line; students who own the method make one clean move — tilt the axes to match the hill — and the problem collapses into two lines of kinematics. That single move is the archetype. This article builds it once, carefully: the tilted-axis master pattern, the range and flight-time results, the maximum-range geometry (hiding a beautiful bisection), the up-slope versus down-slope asymmetry, and the perpendicular-impact condition JEE-Advanced keeps returning to. Learn one tilt, win a family of questions.

Key takeaways
  • A projectile on an incline of angle β\beta is solved by tilting the axes: xx along the slope, yy perpendicular, launch angle α\alpha measured from the incline.
  • Gravity splits into ax=−gsin⁡βa_x = -g\sin\beta along the slope and ay=−gcos⁡βa_y = -g\cos\beta across it. Both directions accelerate: that is the whole novelty.
  • Time of flight T=2usin⁡αgcos⁡βT = \dfrac{2u\sin\alpha}{g\cos\beta} — the same TT whether you fire up or down the slope.
  • Range along the slope: R=2u2sin⁡αcos⁡(α+β)gcos⁡2βR = \dfrac{2u^2\sin\alpha\cos(\alpha+\beta)}{g\cos^2\beta} up the incline; swap β→−β\beta \to -\beta for down.
  • Maximum range up is Rmax⁡=u2g(1+sin⁡β)R_{\max} = \dfrac{u^2}{g(1+\sin\beta)}, when the launch bisects incline and vertical: α=45∘−β/2\alpha = 45^\circ - \beta/2.
  • Key idea: rotate the axes so the incline is the floor — then it is ordinary projectile kinematics with gcos⁡βg\cos\beta across the slope and gsin⁡βg\sin\beta along it.
The core insight

Choosing axes along and perpendicular to the incline turns a projectile-on-a-slope problem into standard two-component kinematics — with the single new feature that gravity now has a component in both directions, −gsin⁡β-g\sin\beta along the slope and −gcos⁡β-g\cos\beta across it.

Where this lives today

The ski jump is this article built at hillside scale. Jumpers leave the table at 85–105 km/h and fly 100+ metres, yet land with impacts gentler than a gym-class hop — the landing hill is profiled to sit only a few degrees below the flight path at touchdown, keeping the perpendicular landing velocity (the usin⁡αu\sin\alpha of the impact derivation, in reverse) tiny even at huge total speed. The same mathematics runs through artillery range tables, which carry slope corrections up and down valley walls, and golf's "plays-like" distances on elevated greens. Wherever a parabola meets a tilted floor, equation (3) is on duty.

The setup

Geometry first, because in an archetype the geometry is the physics. A plane is inclined at angle β\beta. From a point O on the slope, a projectile is launched at speed uu, at an angle α\alpha — the convention that decides everything — measured from the incline surface, not the horizontal. It returns to the slope at P; the distance OP along the slope is the range RR.

Figure
Projectile on an incline — tilted axes and the two components of gravity
β O P u α x (up slope) y g g sinβ (down slope) g cosβ (into slope) still a parabola — the floor moved, not gravity Launch angle α is measured FROM the incline; range R = OP along the slope

Now the master move. Axes may point anywhere — the physics cannot care. On flat ground the smart choice is horizontal–vertical, because gravity then lives in one component. On an incline, take xx along the slope (up-slope positive) and yy perpendicular to it, because the question is asked along the slope: landing means y=0y = 0, and the range is just xx at that moment. The price of this convenience is small and fixed: gravity, still straight down, no longer aligns with either axis. It splits into two components, exactly like a weight on an inclined plane in the laws-of-motion chapter:

ax=−gsin⁡β,ay=−gcos⁡β(1)a_x = -g\sin\beta, \qquad a_y = -g\cos\beta \qquad (1)

where: β\beta — the incline angle; the minus signs say both components oppose the positive directions. Read it physically: across the slope the projectile feels a diluted gravity gcos⁡βg\cos\beta, which curves the path back to the surface. Along the slope it feels a persistent backward tug gsin⁡βg\sin\beta — so, unlike flat ground, the along-floor velocity is no longer constant. That sentence is the archetype's most common mark-loser, and the whole reason it deserves its own module. The initial velocity resolves familiarly: ux=ucos⁡αu_x = u\cos\alpha, uy=usin⁡αu_y = u\sin\alpha. Both directions now run ordinary constant-acceleration kinematics — two independent suvat problems sharing one clock.

The master solution pattern

Every incline question begins identically: tilt the axes, write the two velocity and two acceleration components, deploy standard kinematics in each direction. The landing condition y=0y = 0 hands you the time of flight; substituting it into x(t)x(t) hands you the range.

Derivation ATime of flight and range along the incline

We derive the two master results — the time of flight and the range along the slope — using tilted axes, exactly as a JEE examiner expects the work laid out. The strategy: treat the perpendicular direction as a self-contained "vertical" problem with effective gravity gcos⁡βg\cos\beta to get TT, then feed that time into the along-slope direction, which decelerates uniformly under gsin⁡βg\sin\beta. Watch the launch-angle convention — α\alpha is from the incline throughout — and the along-slope acceleration, which beginners are tempted to set to zero.

Step 1. Set up both directions. Perpendicular to the incline: initial velocity usin⁡αu\sin\alpha, acceleration −gcos⁡β-g\cos\beta. Along the incline: initial velocity ucos⁡αu\cos\alpha, acceleration −gsin⁡β-g\sin\beta. Why: this is the entire content of "tilting the axes" — after this step there is no incline left, only two straight-line kinematics problems sharing a clock.

Step 2. Position perpendicular to the slope:

y(t)=usin⁡α t−12gcos⁡β t2y(t) = u\sin\alpha\, t - \tfrac{1}{2}g\cos\beta\, t^2

Step 3. Landing means y=0y = 0 (with t≠0t \neq 0). Factor out tt:

T=2usin⁡αgcos⁡βT = \frac{2u\sin\alpha}{g\cos\beta}

Why: this is the flat-ground flight time with g→gcos⁡βg \to g\cos\beta — the across-slope motion is a complete little projectile problem of its own, living in a world where gravity is gcos⁡βg\cos\beta.

Step 4. Position along the slope:

x(t)=ucos⁡α t−12gsin⁡β t2x(t) = u\cos\alpha\, t - \tfrac{1}{2}g\sin\beta\, t^2

Step 5. Substitute t=Tt = T and simplify:

R=2u2sin⁡αgcos⁡2β(cos⁡αcos⁡β−sin⁡αsin⁡β)=2u2sin⁡α cos⁡(α+β)gcos⁡2βR = \frac{2u^2\sin\alpha}{g\cos^2\beta}\left(\cos\alpha\cos\beta - \sin\alpha\sin\beta\right) = \frac{2u^2\sin\alpha\,\cos(\alpha+\beta)}{g\cos^2\beta}

Why: the bracket compressed by the addition formula for cos⁡(α+β)\cos(\alpha+\beta) — sensible, since α+β\alpha + \beta is exactly the launch angle above the horizontal. *Verified: β=0\beta = 0 gives T=2usin⁡α/gT = 2u\sin\alpha/g ✓ and R=u2sin⁡2α/gR = u^2\sin 2\alpha/g ✓. Numbers: u=20u = 20, α=β=30∘\alpha = \beta = 30^\circ, g=10g = 10: T=2.31T = 2.31 s, R=200/7.5=26.7R = 200/7.5 = 26.7 m.*

The time of flight contains only across-slope quantities — "how long until it comes back to the surface" is purely a perpendicular-direction question:

T=2usin⁡αgcos⁡β(2)T = \frac{2u\sin\alpha}{g\cos\beta} \qquad (2)

where: usin⁡αu\sin\alpha — the launch component away from the slope; gcos⁡βg\cos\beta — the gravity component pressing back toward it. Two consequences worth caching: TT is longer than the flat-ground flight time for the same α\alpha (dividing by cos⁡β<1\cos\beta < 1), and TT is identical whether you launch up the slope or down it — the along-slope direction never enters.

R=2u2sin⁡α cos⁡(α+β)gcos⁡2β(3)R = \frac{2u^2\sin\alpha\,\cos(\alpha+\beta)}{g\cos^2\beta} \qquad (3)

where: α+β\alpha+\beta — the launch angle above the horizontal; cos⁡2β\cos^2\beta — one factor from the flight time, one from the along-slope geometry. The cos⁡(α+β)\cos(\alpha+\beta) factor announces the up-slope penalty: as the total elevation approaches 90∘90^\circ, the range dies — fire too steeply over a steep hill and you land almost back at your feet.

quantityup the inclinedown the incline
time of flightT=2usin⁡αgcos⁡βT = \dfrac{2u\sin\alpha}{g\cos\beta}same — TT never sees the slope direction
range along slopeR=2u2sin⁡αcos⁡(α+β)gcos⁡2βR = \dfrac{2u^2\sin\alpha\cos(\alpha+\beta)}{g\cos^2\beta}R=2u2sin⁡αcos⁡(α−β)gcos⁡2βR = \dfrac{2u^2\sin\alpha\cos(\alpha-\beta)}{g\cos^2\beta}
maximum rangeRmax⁡=u2g(1+sin⁡β)R_{\max} = \dfrac{u^2}{g(1+\sin\beta)} at α=45∘−β2\alpha = 45^\circ - \dfrac{\beta}{2}Rmax⁡=u2g(1−sin⁡β)R_{\max} = \dfrac{u^2}{g(1-\sin\beta)} at α=45∘+β2\alpha = 45^\circ + \dfrac{\beta}{2}

Every "down" entry is the "up" formula with β→−β\beta \to -\beta — one substitution instead of four formulas.

Go deeper · Derivation B · 1 minMaximum range and the bisection rule
Derivation BMaximum range and the bisection rule

We derive the launch angle that maximises the range up the incline, and the maximum range itself — the most-quoted result of this archetype. The strategy is an algebraic classic worth owning: the product sin⁡αcos⁡(α+β)\sin\alpha\cos(\alpha+\beta) in equation (3) is awkward to maximise as written, so we convert it into a sum via 2sin⁡Acos⁡B=sin⁡(A+B)+sin⁡(A−B)2\sin A\cos B = \sin(A+B) + \sin(A-B), after which the α\alpha-dependence sits inside a single sine. Watch how β\beta ends up split evenly on both sides of the launch direction — beautiful geometry hiding in the algebra.

Step 1. Apply the product-to-sum identity with A=αA = \alpha, B=α+βB = \alpha + \beta:

2sin⁡αcos⁡(α+β)=sin⁡(2α+β)−sin⁡β2\sin\alpha\cos(\alpha+\beta) = \sin(2\alpha+\beta) - \sin\beta

Step 2. The range becomes

R=u2gcos⁡2β[sin⁡(2α+β)−sin⁡β]R = \frac{u^2}{g\cos^2\beta}\left[\sin(2\alpha+\beta) - \sin\beta\right]

Why: everything except sin⁡(2α+β)\sin(2\alpha+\beta) is fixed by the problem — uu, gg, β\beta are given. Maximising RR over the launch angle is now one glance: push the sine to its ceiling of 1.

Step 3. Maximum when sin⁡(2α+β)=1\sin(2\alpha+\beta) = 1, i.e. 2α+β=90∘2\alpha + \beta = 90^\circ:

α=45∘−β2\alpha = 45^\circ - \frac{\beta}{2}

Why this is a bisection: from the horizontal, the launch sits at α+β=45∘+β/2\alpha + \beta = 45^\circ + \beta/2 — exactly halfway between the incline (at β\beta) and the vertical (at 90∘90^\circ). On flat ground this reproduces the famous 45∘45^\circ, which bisects horizontal and vertical.

Step 4. Substitute sin⁡(2α+β)=1\sin(2\alpha+\beta) = 1 and use cos⁡2β=(1+sin⁡β)(1−sin⁡β)\cos^2\beta = (1+\sin\beta)(1-\sin\beta):

Rmax⁡=u2(1−sin⁡β)gcos⁡2β=u2g(1+sin⁡β)R_{\max} = \frac{u^2(1-\sin\beta)}{g\cos^2\beta} = \frac{u^2}{g(1+\sin\beta)}

Step 5. Down the incline, replace β→−β\beta \to -\beta: Rmax⁡down=u2g(1−sin⁡β)R_{\max}^{\text{down}} = \dfrac{u^2}{g(1-\sin\beta)} at α=45∘+β/2\alpha = 45^\circ + \beta/2. Verified: β=0\beta = 0 gives u2/gu^2/g at 45∘45^\circ ✓. Numbers: u=30u = 30, β=30∘\beta = 30^\circ, g=10g = 10: up 900/15=60900/15 = 60 m; down 900/5=180900/5 = 180 m — ratio (1+sin⁡β)/(1−sin⁡β)=3(1+\sin\beta)/(1-\sin\beta) = 3 exactly.

Figure
Maximum range geometry — the optimal launch bisects slope and vertical
O vertical optimal u α = 45° − β/2 45° − β/2 again launch bisects incline ↔ vertical β P R max up = u²/(g(1+sinβ)) down-slope: R max = u²/(g(1−sinβ)) Same u: downhill maximum beats uphill maximum by the factor (1+sinβ)/(1−sinβ)

The ground-frame alternative — and when each frame wins

Nothing forces the tilt. Keep horizontal–vertical axes, write the ordinary trajectory y=xtan⁡θ−gx22u2cos⁡2θy = x\tan\theta - \dfrac{gx^2}{2u^2\cos^2\theta} with θ=α+β\theta = \alpha + \beta, and intersect it with the incline line y=xtan⁡βy = x\tan\beta. The non-zero root gives xP=2u2cos⁡2θ (tan⁡θ−tan⁡β)gx_P = \dfrac{2u^2\cos^2\theta\,(\tan\theta - \tan\beta)}{g}, and R=xP/cos⁡βR = x_P/\cos\beta — chase the trigonometry and it reproduces equation (3) exactly. When does each frame win? Tilted axes, whenever the question speaks the slope's language: range along the incline, time to return to the surface, perpendicular impact. Ground frame, when it speaks the horizontal's: "at what horizontal distance", "at the highest point above the ground" — since highest above ground means the ground-frame vertical velocity vanishes, not the tilted vyv_y. Fluency means choosing in five seconds, not solving both.

The perpendicular-impact condition

JEE-Advanced's favourite twist: the projectile strikes the incline perpendicularly. In tilted axes this is one clean sentence: at impact the along-slope velocity has died, vx(T)=0v_x(T) = 0.

Go deeper · Derivation C · 1 minStriking the incline at right angles
Derivation CStriking the incline at right angles

We derive the launch condition for the projectile to hit the incline perpendicularly — a two-line argument in tilted axes that costs a page in the ground frame, which is precisely why examiners set it. The strategy: write both velocity components in time, impose vx=0v_x = 0 at the landing moment t=Tt = T, and watch a clean relation between α\alpha and β\beta fall out — with the impact speed as a free bonus.

Step 1. The along-slope velocity decays under the tug gsin⁡βg\sin\beta:

vx(t)=ucos⁡α−gsin⁡β tv_x(t) = u\cos\alpha - g\sin\beta\, t

Step 2. Impose vx=0v_x = 0 at the landing time T=2usin⁡αgcos⁡βT = \dfrac{2u\sin\alpha}{g\cos\beta} from equation (2):

ucos⁡α=gsin⁡β⋅2usin⁡αgcos⁡βu\cos\alpha = g\sin\beta \cdot \frac{2u\sin\alpha}{g\cos\beta}

Step 3. Cancel uu and gg, gather the trigonometry:

cot⁡α=2tan⁡β\cot\alpha = 2\tan\beta

Why the condition only involves angles: launch speed and gravity set the scale of the motion, but "does the velocity end up perpendicular?" is a question about directions — scales must cancel, and they do.

Step 4. The impact speed. At landing, vy(T)=usin⁡α−gcos⁡β T=−usin⁡αv_y(T) = u\sin\alpha - g\cos\beta\,T = -u\sin\alpha, so the projectile strikes with speed

vimpact=usin⁡αv_{\text{impact}} = u\sin\alpha

Why the symmetry: the across-slope motion is a full "up and back" in its own diluted gravity, so it returns through y=0y = 0 with its launch component reversed — the usual up–down symmetry. *Verified: for β=45∘\beta = 45^\circ: cot⁡α=2\cot\alpha = 2, α≈26.6∘\alpha \approx 26.6^\circ. With u=10u = 10, g=10g = 10: T=22/5≈1.26T = 2\sqrt{2/5} \approx 1.26 s; vx(T)=8.94−8.94=0v_x(T) = 8.94 - 8.94 = 0 ✓; impact speed 10/5≈4.4710/\sqrt5 \approx 4.47 m/s =usin⁡α= u\sin\alpha ✓.*

Limiting cases

caseresultmeaning
β=0\beta = 0T=2usin⁡αgT = \dfrac{2u\sin\alpha}{g}, R=u2sin⁡2αgR = \dfrac{u^2\sin 2\alpha}{g}, Rmax⁡=u2gR_{\max} = \dfrac{u^2}{g} at 45∘45^\circflat ground recovered — every formula must pass this check
α+β=90∘\alpha + \beta = 90^\circR=0R = 0launched vertically: straight up, straight back to the launch point
α=90∘\alpha = 90^\circR=−2u2sin⁡βgcos⁡2β<0R = -\dfrac{2u^2\sin\beta}{g\cos^2\beta} < 0fired perpendicular to the slope, it lands below O — the gsin⁡βg\sin\beta tug wins
β→90∘\beta \to 90^\circRmax⁡up→u22gR_{\max}^{\text{up}} \to \dfrac{u^2}{2g}a vertical "wall": max range up = max height of a vertical throw — same problem
up vs down at same α\alphaRdownRup=cos⁡(α−β)cos⁡(α+β)\dfrac{R_{\text{down}}}{R_{\text{up}}} = \dfrac{\cos(\alpha-\beta)}{\cos(\alpha+\beta)}downhill always wins; the ratio blows up as α+β→90∘\alpha + \beta \to 90^\circ

Worked examples

1 · Board level — the direct crank (JEE-Main pattern)

A particle is projected at u=20 m/su = 20\ \mathrm{m/s} at 30∘30^\circ to an incline of angle 30∘30^\circ, up the slope. Find the time of flight and the range along the incline. Take g=10 m/s2g = 10\ \mathrm{m/s^2}.

Step 1. Tilt the axes: ux=17.3 m/su_x = 17.3\ \mathrm{m/s}, uy=10 m/su_y = 10\ \mathrm{m/s}; ax=−10sin⁡30∘=−5 m/s2a_x = -10\sin 30^\circ = -5\ \mathrm{m/s^2}, ay=−10cos⁡30∘=−8.66 m/s2a_y = -10\cos 30^\circ = -8.66\ \mathrm{m/s^2}.

Step 2. Time of flight: T=2usin⁡αgcos⁡β=2(20)(0.5)10(0.866)=2.31 sT = \dfrac{2u\sin\alpha}{g\cos\beta} = \dfrac{2(20)(0.5)}{10(0.866)} = \boxed{2.31\ \mathrm{s}}.

Step 3. Range along the slope: R=ucos⁡α T−12gsin⁡β T2=40.0−13.3=26.7 mR = u\cos\alpha\,T - \tfrac12 g\sin\beta\,T^2 = 40.0 - 13.3 = \boxed{26.7\ \mathrm{m}}.

Step 4. Cross-check with (3): R=2(400)(0.5)cos⁡60∘10(0.75)=2007.5=26.7 mR = \dfrac{2(400)(0.5)\cos 60^\circ}{10(0.75)} = \dfrac{200}{7.5} = 26.7\ \mathrm{m} ✓. Note what Step 3 quietly displays: the naive constant-vxv_x answer would be 4040 m — the gsin⁡βg\sin\beta term claws back a full third of it.

2 · Board level — best throw up, best throw down

A footballer on a 30∘30^\circ hillside can kick at u=30 m/su = 30\ \mathrm{m/s}. Find the farthest he can send the ball (a) up the slope and (b) down the slope, and the launch angle for each. (g=10 m/s2g = 10\ \mathrm{m/s^2}.)

Step 1. Up: Rmax⁡=u2g(1+sin⁡β)=90015=60 mR_{\max} = \dfrac{u^2}{g(1+\sin\beta)} = \dfrac{900}{15} = \boxed{60\ \mathrm{m}}, at α=45∘−β/2=30∘\alpha = 45^\circ - \beta/2 = 30^\circ from the incline (60∘60^\circ from horizontal — bisecting slope and vertical ✓).

Step 2. Down: Rmax⁡=u2g(1−sin⁡β)=9005=180 mR_{\max} = \dfrac{u^2}{g(1-\sin\beta)} = \dfrac{900}{5} = \boxed{180\ \mathrm{m}}, at α=45∘+β/2=60∘\alpha = 45^\circ + \beta/2 = 60^\circ from the incline.

Step 3. The asymmetry: downhill beats uphill by 1+sin⁡30∘1−sin⁡30∘=3\dfrac{1+\sin 30^\circ}{1-\sin 30^\circ} = 3 — same boot, three times the reach. On a hillside, geometry is destiny.

3 · Competitive level — perpendicular impact (JEE-Advanced pattern, ~3 minutes)

A ball projected from the foot of a 45∘45^\circ incline strikes it perpendicularly. If u=10 m/su = 10\ \mathrm{m/s} and g=10 m/s2g = 10\ \mathrm{m/s^2}, find (a) the launch angle α\alpha from the incline, (b) the time of flight, (c) the impact speed.

Step 1. Perpendicular impact means vx=0v_x = 0 at landing: cot⁡α=2tan⁡β=2\cot\alpha = 2\tan\beta = 2, so tan⁡α=12\tan\alpha = \tfrac12, α=tan⁡−1(0.5)≈26.6∘\boxed{\alpha = \tan^{-1}(0.5) \approx 26.6^\circ}; then sin⁡α=1/5\sin\alpha = 1/\sqrt5, cos⁡α=2/5\cos\alpha = 2/\sqrt5.

Step 2. Time of flight: T=2usin⁡αgcos⁡β=2(10)(1/5)10(1/2)=225=1.26 sT = \dfrac{2u\sin\alpha}{g\cos\beta} = \dfrac{2(10)(1/\sqrt5)}{10(1/\sqrt2)} = \dfrac{2\sqrt2}{\sqrt5} = \boxed{1.26\ \mathrm{s}}.

Step 3. Check the defining condition: vx(T)=205−10⋅12⋅225=0v_x(T) = \dfrac{20}{\sqrt5} - 10\cdot\dfrac{1}{\sqrt2}\cdot\dfrac{2\sqrt2}{\sqrt5} = 0 ✓.

Step 4. Impact speed = the surviving perpendicular component: ∣vy(T)∣=usin⁡α=25≈4.5 m/s|v_y(T)| = u\sin\alpha = \boxed{2\sqrt5 \approx 4.5\ \mathrm{m/s}}. Timing note: with cot⁡α=2tan⁡β\cot\alpha = 2\tan\beta cached this is 90 seconds of arithmetic; deriving it live costs one extra minute. Without tilted axes it is a seven-minute swamp. Budget ~3 min and bank the surplus.

4 · Competitive level — same launch, both directions (JEE-Advanced comparison, ~3 minutes)

From a point on a 30∘30^\circ incline, two balls are thrown at u=20 m/su = 20\ \mathrm{m/s}, each at 30∘30^\circ to the incline — one up-slope, one down. Find the ratio of flight times and of ranges. (g=10 m/s2g = 10\ \mathrm{m/s^2}.)

Step 1. Flight times. Equation (2) contains no trace of the slope direction: Tup=Tdown=2.31 sT_{\text{up}} = T_{\text{down}} = 2.31\ \mathrm{s}, ratio 1:1\boxed{1:1} — the planted trap option cos⁡(α+β)/cos⁡(α−β)\cos(\alpha+\beta)/\cos(\alpha-\beta) belongs to the ranges, not the times.

Step 2. Up-slope range (from Example 1): Rup=26.7 mR_{\text{up}} = 26.7\ \mathrm{m}. Down-slope, replace β→−β\beta \to -\beta in (3): Rdown=2(400)(0.5)cos⁡0∘10(0.75)=53.3 mR_{\text{down}} = \dfrac{2(400)(0.5)\cos 0^\circ}{10(0.75)} = \boxed{53.3\ \mathrm{m}}.

Step 3. Ratio: RdownRup=cos⁡(α−β)cos⁡(α+β)=1cos⁡60∘=2\dfrac{R_{\text{down}}}{R_{\text{up}}} = \dfrac{\cos(\alpha-\beta)}{\cos(\alpha+\beta)} = \dfrac{1}{\cos 60^\circ} = \boxed{2} — twice as far along the slope, in the same airtime. Timing note: ~2.5 minutes with the closed formulas and the β→−β\beta \to -\beta rule; re-deriving each range from components doubles it. The instant kill: airtime equality is free from equation (2) — never compute it twice.

Exam traps

Measuring α\alpha from the wrong line. These formulas take α\alpha from the incline. Given the angle from the horizontal — call it θ\theta — convert first: α=θ−β\alpha = \theta - \beta. Feeding a horizontal-referenced angle into an incline-referenced formula is the archetype's most reliable mark-shredder.

Setting ax=0a_x = 0. Flat-ground reflex. On the incline both components accelerate. If your range came from "ucos⁡α×Tu\cos\alpha \times T", it is wrong — always too large, and the error grows with β\beta.

Using R=u2sin⁡2α/gR = u^2\sin 2\alpha/g on a slope. That formula presumes launch and landing at the same level. On an incline it answers nothing; examiners plant it among the options anyway.

cos⁡β\cos\beta versus cos⁡2β\cos^2\beta. The time of flight carries one power of cos⁡β\cos\beta; the range carries two. Both slips are dimensionally clean, so no audit saves you — cache the pair as "TT: one cos, RR: two".

Along-slope range versus horizontal distance. RR is along the incline; horizontal separation is Rcos⁡βR\cos\beta. Read the question's last line twice.

Sign discipline downhill. Either flip the xx-axis to point down-slope (ax=+gsin⁡βa_x = +g\sin\beta then helps the motion) or substitute β→−β\beta \to -\beta in the closed formulas — never mix the two conventions in one solution.

Which gg? JEE papers almost always declare g=10 m/s2g = 10\ \mathrm{m/s^2} — use what is stated, in both components.

Origins · 1 minEvangelista Torricelli and how this was discovered
ET
Evangelista Torricelli
1608–1647 · Florence, successor to Galileo

Torricelli inherited Galileo's chair in Florence and pushed his master's parabola further than anyone alive. His De motu proiectorum (1644) worked out where projectiles land on arbitrary planes and proved a stunning theorem: all trajectories from a point at the same speed are bounded by one master parabola — the parabola of safety. Nothing outside it can be hit; everything inside can, by two angles. Gunners used his tables for two centuries. The same Torricelli gave physics the barometer, the first sustained vacuum, and the efflux law for jets from a tank.

History
1638
— Galileo's Two New Sciences proves the projectile path is a parabola, compounding uniform horizontal motion with free fall.
1644
— Torricelli's De motu proiectorum extends the parabola to inclined planes and finds the envelope of trajectories — the parabola of safety.
1687
— Newton's Principia grounds the kinematic picture in F=maF = ma and universal gravitation.
1900
s — Exterior ballistics adds air resistance numerically; the vacuum parabola remains the first-order tool for mountain artillery tables.
2000
s — Ski-flying hill certifications specify landing-slope profiles so jumpers meet the ground nearly tangentially — incline-projectile geometry as safety engineering.

Going further

Texts. H.C. Verma, Concepts of Physics Vol. 1, Ch. 3 · D.C. Pandey, Understanding Physics: Mechanics 1, projectile chapter (the standard JEE drill set) · Irodov, Problems in General Physics, §1.3 for stretch versions.

Provenance. Standard JEE canon. A verifier should recompute: the β=0\beta = 0 collapse of (2) and (3); Example 1's T=2.31T = 2.31 s, R=26.7R = 26.7 m (both routes); Example 2's 60 m and 180 m (ratio 3); Example 3's α=tan⁡−1(0.5)\alpha = \tan^{-1}(0.5), T=22/5=1.26T = 2\sqrt2/\sqrt5 = 1.26 s, impact speed 252\sqrt5 m/s; Example 4's equal airtimes and range ratio 2; the identity u2(1−sin⁡β)/(gcos⁡2β)=u2/(g(1+sin⁡β))u^2(1-\sin\beta)/(g\cos^2\beta) = u^2/(g(1+\sin\beta)).

Prerequisites. Projectile Motion · Projectile from a Height · Components & Resolution of Vectors. Leads to. The Block-on-Incline Family · Limiting & Extreme Cases (technique).

Why tilt the axes at all — is the ground frame wrong?

Not wrong, just expensive for most incline questions. The landing condition on tilted axes is the one-symbol statement y=0y = 0; in the ground frame it is the intersection of a parabola with a slanted line — a simultaneous-equation chore. The trade is that gravity splits into two components, but that costs one line and pays back everywhere else. Use the ground frame only when the question is phrased horizontally ("horizontal distance", "highest point above the ground"); deciding which language the question speaks is the first five seconds of the solution.

Is the trajectory still a parabola when the ground is inclined?

Yes — the path in space is set by gravity, not by the floor. Gravity is still uniform and straight down, so the trajectory is the same parabola it would be over flat ground; the incline merely slices that parabola at a different landing point. What changes in tilted coordinates is the bookkeeping: both coordinates now carry quadratic time-dependence. The curve never changed; your description of it did.

Why is the time of flight the same up the slope and down the slope?

Because "when does it come back to the surface?" lives entirely in the perpendicular direction — launch component usin⁡αu\sin\alpha, restoring acceleration gcos⁡βg\cos\beta — and neither knows which way along the slope you fired. The slope direction decides where you land, not when. Equal airtime is a reliable free mark in comparison questions — and a planted trap ratio in MCQ options.

How do I convert if the question gives the launch angle from the horizontal?

Subtract the slope: a throw at θ\theta above the horizontal has incline-referenced angle α=θ−β\alpha = \theta - \beta. Convert before touching any formula — every formula in this archetype assumes the incline reference. The reverse slip also bites: the optimal launch is 45∘−β/245^\circ - \beta/2 from the incline but 45∘+β/245^\circ + \beta/2 from the horizontal — quote the one the question asked for.

Where does the greatest distance from the incline occur, and how large is it?

At half the flight time, t=T/2t = T/2 — the across-slope motion is symmetric, so the "peak" above the slope sits midway. The maximum perpendicular distance is d=(usin⁡α)22gcos⁡βd = \dfrac{(u\sin\alpha)^2}{2g\cos\beta} — the maximum-height formula with g→gcos⁡βg \to g\cos\beta. Careful with words: this is the farthest point from the slope surface; the highest point above the ground is a different event at a different time.

Do I need to memorise the incline range formula, or derive it each time?

For JEE-Main, cache four things: the two acceleration components, the flight time 2usin⁡α/(gcos⁡β)2u\sin\alpha/(g\cos\beta), and the maximum-range pair u2/(g(1±sin⁡β))u^2/(g(1\pm\sin\beta)) with the bisection rule α=45∘∓β/2\alpha = 45^\circ \mp \beta/2; the full range expression (3) is one substitution away. For JEE-Advanced, practise the derivation to a 90-second reflex — Advanced rarely asks the formula straight; it asks perpendicular impacts, ratios, and hybrids where only the method survives.

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Where this leads