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Newton's Laws with Calculus | Study Mondo
Topics / Dynamics / Newton's Laws with Calculus Newton's Laws with Calculus Force, mass, and acceleration relationships using derivatives and integrals
๐ฏ โญ INTERACTIVE LESSON
Try the Interactive Version! Learn step-by-step with practice exercises built right in.
Start Interactive Lesson โ Newton's Laws with Calculus
Newton's Second Law
Vector form:
F โ n e t = m a โ = m d v โ d t = m d 2 r โ d t 2 \vec{F}_{net} = m\vec{a} = m\frac{d\vec{v}}{dt} = m\frac{d^2\vec{r}}{dt^2} F
๐ Practice Problems
1 Problem 1medium โ Question:A 2.0 kg block experiences a time-dependent force F(t) = (8 - 2t) N for 0 โค t โค 4 s. The block starts from rest. Find: (a) the impulse delivered to the block, (b) the final velocity, and (c) the work done by the force.
๐ก Show Solution Given:
m = 2.0 kg
F(t) = 8 - 2t N
vโ = 0
Time interval: [0, 4] s
(a) Impulse:
J = โซ 0 4 F ( t ) โ
Explain using: ๐ Simple words ๐ Analogy ๐จ Visual desc. ๐ Example ๐ก Explain
๐งช Practice Lab Interactive practice problems for Newton's Laws with Calculus
โพ ๐ Related Topics in Dynamicsโ Frequently Asked QuestionsWhat is Newton's Laws with Calculus?โพ Force, mass, and acceleration relationships using derivatives and integrals
How can I study Newton's Laws with Calculus effectively?โพ Start by reading the study notes and working through the examples on this page. Then use the flashcards to test your recall. Practice with the 3 problems provided, checking solutions as you go. Regular review and active practice are key to retention.
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What course covers Newton's Laws with Calculus?โพ Newton's Laws with Calculus is part of the AP Physics C: Mechanics course on Study Mondo, specifically in the Dynamics section. You can explore the full course for more related topics and practice resources.
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๐ก Study Tipsโ Work through examples step-by-step โ Practice with flashcards daily โ Review common mistakes n e t โ
=
Component form:
F x = m d v x d t , F y = m d v y d t , F z = m d v z d t F_x = m\frac{dv_x}{dt}, \quad F_y = m\frac{dv_y}{dt}, \quad F_z = m\frac{dv_z}{dt} F x โ = m d t d v x โ โ , F y โ = m d t d v y โ โ , F z โ = m d t d v z โ โ
Impulse-Momentum Theorem From Newton's second law:
F โ = d p โ d t \vec{F} = \frac{d\vec{p}}{dt} F = d t d p โ โ
where momentum p โ = m v โ \vec{p} = m\vec{v} p โ = m v .
Integrating both sides:
โซ t 1 t 2 F โ โ d t = โซ t 1 t 2 d p โ d t โ d t = p โ 2 โ p โ 1 = ฮ p โ \int_{t_1}^{t_2} \vec{F} \, dt = \int_{t_1}^{t_2} \frac{d\vec{p}}{dt} \, dt = \vec{p}_2 - \vec{p}_1 = \Delta \vec{p} โซ t 1 โ t 2 โ โ F d t = โซ t 1 โ t 2 โ โ d t p โ 2 โ โ p โ 1 โ = ฮ p โ
Impulse:
J โ = โซ t 1 t 2 F โ โ d t = ฮ p โ \vec{J} = \int_{t_1}^{t_2} \vec{F} \, dt = \Delta \vec{p} J = โซ t 1 โ t 2 โ โ F d t = ฮ p โ
Variable Force Example If F ( t ) = F 0 cos โก ( ฯ t ) F(t) = F_0\cos(\omega t) F ( t ) = F 0 โ cos ( ฯ t ) for time 0 0 0 to T = ฯ / ( 2 ฯ ) T = \pi/(2\omega) T = ฯ / ( 2 ฯ ) :
J = โซ 0 T F 0 cos โก ( ฯ t ) โ d t = F 0 ฯ sin โก ( ฯ t ) โฃ 0 T = F 0 ฯ J = \int_0^T F_0\cos(\omega t) \, dt = \frac{F_0}{\omega}\sin(\omega t)\Big|_0^T = \frac{F_0}{\omega} J = โซ 0 T โ F 0 โ cos ( ฯ t ) d t = ฯ F 0 โ โ sin ( ฯ t ) โ ฯ F 0 โ โ
Variable Mass Systems For systems where mass changes with time (rockets):
F โ e x t = d p โ d t = d ( m v โ ) d t = m d v โ d t + v โ d m d t \vec{F}_{ext} = \frac{d\vec{p}}{dt} = \frac{d(m\vec{v})}{dt} = m\frac{d\vec{v}}{dt} + \vec{v}\frac{dm}{dt} F e x t โ = d t d p โ โ = d t d ( m v ) โ = m d t d v โ + v d t d m โ
Rocket equation:
m d v d t = โ v r e l d m d t + F e x t m\frac{dv}{dt} = -v_{rel}\frac{dm}{dt} + F_{ext} m d t d v โ = โ v re l โ d t d m โ + F e x t โ
where v r e l v_{rel} v re l โ is exhaust velocity relative to rocket.
For no external forces and integrating:
ฮ v = v r e l ln โก m 0 m f \Delta v = v_{rel}\ln\frac{m_0}{m_f} ฮ v = v re l โ ln m f โ m 0 โ โ
(Tsiolkovsky rocket equation)
Drag Forces Linear drag: F d = โ b v F_d = -bv F d โ = โ b v
m d v d t = โ b v m\frac{dv}{dt} = -bv m d t d v โ = โ b v
Solution: v ( t ) = v 0 e โ b t / m v(t) = v_0e^{-bt/m} v ( t ) = v 0 โ e โ b t / m
Quadratic drag: F d = โ c v 2 F_d = -cv^2 F d โ = โ c v 2
m d v d t = โ c v 2 m\frac{dv}{dt} = -cv^2 m d t d v โ = โ c v 2
Separating variables:
โซ v 0 v d v โฒ v โฒ 2 = โ c m โซ 0 t d t โฒ \int_{v_0}^v \frac{dv'}{v'^2} = -\frac{c}{m}\int_0^t dt' โซ v 0 โ v โ v โฒ2 d v โฒ โ = โ m c โ โซ 0 t โ d t โฒ
v ( t ) = v 0 1 + c v 0 t m v(t) = \frac{v_0}{1 + \frac{cv_0t}{m}} v ( t ) = 1 + m c v 0 โ t โ v 0 โ โ
Falling with Air Resistance Equation of motion:
m d v d t = m g โ b v m\frac{dv}{dt} = mg - bv m d t d v โ = m g โ b v
Terminal velocity: v t = m g b v_t = \frac{mg}{b} v t โ = b m g โ
Rewrite as:
d v d t = g โ b m v = b m ( v t โ v ) \frac{dv}{dt} = g - \frac{b}{m}v = \frac{b}{m}(v_t - v) d t d v โ = g โ m b โ v = m b โ ( v t โ โ v )
Solution:
v ( t ) = v t ( 1 โ e โ b t / m ) v(t) = v_t(1 - e^{-bt/m}) v ( t ) = v t โ ( 1 โ e โ b t / m )
Forces in Polar Coordinates Newton's second law in polar coordinates:
Radial direction:
F r = m ( r ยจ โ r ฮธ ห 2 ) F_r = m(\ddot{r} - r\dot{\theta}^2) F r โ = m ( r ยจ โ r ฮธ ห 2 )
Tangential direction:
F ฮธ = m ( r ฮธ ยจ + 2 r ห ฮธ ห ) F_{\theta} = m(r\ddot{\theta} + 2\dot{r}\dot{\theta}) F ฮธ โ = m ( r ฮธ ยจ + 2 r ห ฮธ ห )
Example: Central Force For motion under central force (depends only on r r r ):
F ฮธ = 0 F_{\theta} = 0 F ฮธ โ = 0 , so:
r ฮธ ยจ + 2 r ห ฮธ ห = 0 r\ddot{\theta} + 2\dot{r}\dot{\theta} = 0 r ฮธ ยจ + 2 r ห ฮธ ห = 0
d d t ( r 2 ฮธ ห ) = 0 \frac{d}{dt}(r^2\dot{\theta}) = 0 d t d โ ( r 2 ฮธ ห ) = 0
This means r 2 ฮธ ห = L / m r^2\dot{\theta} = L/m r 2 ฮธ ห = L / m is constant (angular momentum conservation).
d t = โซ 0 4 ( 8 โ 2 t ) โ d t J = \int_0^4 F(t) \, dt = \int_0^4 (8 - 2t) \, dt J = โซ 0 4 โ F ( t ) d t = โซ 0 4 โ ( 8 โ 2 t ) d t
J = [ 8 t โ t 2 ] 0 4 = 32 โ 16 J = \left[8t - t^2\right]_0^4 = 32 - 16 J = [ 8 t โ t 2 ] 0 4 โ = 32 โ 16
J = 16 ย N \cdotp s \boxed{J = 16 \text{ Nยทs}} J = 16 ย N \cdotp s โ
Using impulse-momentum theorem:
J = ฮ p = m ( v f โ v 0 ) J = \Delta p = m(v_f - v_0) J = ฮ p = m ( v f โ โ v 0 โ )
16 = 2.0 ( v f โ 0 ) 16 = 2.0(v_f - 0) 16 = 2.0 ( v f โ โ 0 )
v f = 8.0 ย m/s \boxed{v_f = 8.0 \text{ m/s}} v f โ = 8.0 ย m/s โ
First find position. Using F = ma:
a ( t ) = F m = 8 โ 2 t 2 = 4 โ t a(t) = \frac{F}{m} = \frac{8 - 2t}{2} = 4 - t a ( t ) = m F โ = 2 8 โ 2 t โ = 4 โ t
v ( t ) = โซ 0 t ( 4 โ t โฒ ) โ d t โฒ = 4 t โ t 2 2 v(t) = \int_0^t (4 - t') \, dt' = 4t - \frac{t^2}{2} v ( t ) = โซ 0 t โ ( 4 โ t โฒ ) d t โฒ = 4 t โ 2 t 2 โ
x ( t ) = โซ 0 t ( 4 t โฒ โ t โฒ 2 2 ) d t โฒ = 2 t 2 โ t 3 6 x(t) = \int_0^t \left(4t' - \frac{t'^2}{2}\right) dt' = 2t^2 - \frac{t^3}{6} x ( t ) = โซ 0 t โ ( 4 t โฒ โ 2 t โฒ2 โ ) d t โฒ = 2 t 2 โ 6 t 3 โ
Distance at t = 4:
x ( 4 ) = 2 ( 16 ) โ 64 6 = 32 โ 10.67 = 21.33 ย m x(4) = 2(16) - \frac{64}{6} = 32 - 10.67 = 21.33 \text{ m} x ( 4 ) = 2 ( 16 ) โ 6 64 โ = 32 โ 10.67 = 21.33 ย m
Work:
W = โซ 0 4 F ( t ) โ
v ( t ) โ d t = โซ 0 4 ( 8 โ 2 t ) ( 4 t โ t 2 2 ) d t W = \int_0^4 F(t) \cdot v(t) \, dt = \int_0^4 (8-2t)\left(4t - \frac{t^2}{2}\right) dt W = โซ 0 4 โ F ( t ) โ
v ( t ) d t = โซ 0 4 โ ( 8 โ 2 t ) ( 4 t โ 2 t 2 โ ) d t
Or using work-energy theorem:
W = ฮ K E = 1 2 m v f 2 โ 0 = 1 2 ( 2.0 ) ( 8.0 ) 2 W = \Delta KE = \frac{1}{2}mv_f^2 - 0 = \frac{1}{2}(2.0)(8.0)^2 W = ฮ K E = 2 1 โ m v f 2 โ โ 0 = 2 1 โ ( 2.0 ) ( 8.0 ) 2
W = 64 ย J \boxed{W = 64 \text{ J}} W = 64 ย J โ
2 Problem 2hard โ Question:A rocket of initial mass mโ = 1000 kg burns fuel at rate dm/dt = -10 kg/s with exhaust velocity v_e = 2000 m/s relative to the rocket. Neglecting gravity, find: (a) the thrust force, (b) the acceleration as a function of time, and (c) the velocity after 30 seconds.
๐ก Show Solution Given:
mโ = 1000 kg
dm/dt = -10 kg/s
v_e = 2000 m/s
Ignore gravity
(a) Thrust force:
Rocket equation (thrust):
F t h r u s t = โ v e d m d t F_{thrust} = -v_e \frac{dm}{dt} F t h r u s t โ = โ v e โ d t d m โ
F t h r u s t = โ ( 2000 ) ( โ 10 ) F_{thrust} = -(2000)(-10) F t h r u s t โ = โ ( 2000 ) ( โ 10 )
F t h r u s t = 20 , 000 ย N = 20 ย kN \boxed{F_{thrust} = 20,000 \text{ N} = 20 \text{ kN}} F t h r u s t โ = 20 , 000 ย N = 20 ย kN
(Constant as long as burn rate is constant)
(b) Acceleration as function of time:
Mass at time t:
m ( t ) = m 0 + ( d m d t ) t = 1000 โ 10 t m(t) = m_0 + \left(\frac{dm}{dt}\right)t = 1000 - 10t m ( t ) = m 0 โ + ( d t
Newton's second law:
F = m a F = ma F = ma
20000 = ( 1000 โ 10 t ) a 20000 = (1000 - 10t)a 20000 = ( 1000 โ 10 t ) a
a ( t ) = 20000 1000 โ 10 t = 2000 100 โ t a(t) = \frac{20000}{1000 - 10t} = \frac{2000}{100 - t} a ( t ) = 1000 โ 10 t 20000 โ =
a ( t ) = 2000 100 โ t ย m/s 2 \boxed{a(t) = \frac{2000}{100 - t} \text{ m/s}^2} a ( t ) = 100 โ t 2000 โ ย m/s
(c) Velocity after 30 s:
Using Tsiolkovsky rocket equation:
ฮ v = v e ln โก ( m 0 m f ) \Delta v = v_e \ln\left(\frac{m_0}{m_f}\right) ฮ v = v e โ ln ( m f
At t = 30 s:
m f = 1000 โ 10 ( 30 ) = 700 ย kg m_f = 1000 - 10(30) = 700 \text{ kg} m f โ = 1000 โ 10 ( 30 ) = 700 ย kg
ฮ v = 2000 ln โก ( 1000 700 ) = 2000 ln โก ( 1.429 ) \Delta v = 2000 \ln\left(\frac{1000}{700}\right) = 2000 \ln(1.429) ฮ v = 2000 ln ( 700 1000 โ ) = 2000
ฮ v = 2000 ( 0.357 ) \Delta v = 2000(0.357) ฮ v = 2000 ( 0.357 )
v = 714 ย m/s \boxed{v = 714 \text{ m/s}} v = 714 ย m/s โ
Alternative (integrate acceleration):
v = โซ 0 30 a ( t ) โ d t = โซ 0 30 2000 100 โ t d t v = \int_0^{30} a(t) \, dt = \int_0^{30} \frac{2000}{100-t} dt v = โซ 0 30 โ a ( t ) d t = โซ
v = โ 2000 ln โก ( 100 โ t ) โฃ 0 30 = โ 2000 [ ln โก ( 70 ) โ ln โก ( 100 ) ] v = -2000\ln(100-t)\Big|_0^{30} = -2000[\ln(70) - \ln(100)] v = โ 2000 ln ( 100 โ t ) โ
v = โ 2000 ln โก ( 0.7 ) = 2000 ( 0.357 ) = 714 ย m/s v = -2000\ln(0.7) = 2000(0.357) = 714 \text{ m/s} v = โ 2000 ln ( 0.7 ) = 2000 ( 0.357 ) = 714 ย m/s โ
3 Problem 3medium โ Question:A 5.0 kg object falls through air with drag force F_d = bvยฒ, where b = 0.25 kg/m. Find: (a) the terminal velocity, (b) the differential equation for velocity, and (c) the time to reach 90% of terminal velocity (hint: separate variables and integrate).
๐ก Show Solution Given:
m = 5.0 kg
F_d = bvยฒ where b = 0.25 kg/m
g = 9.8 m/sยฒ
(a) Terminal velocity:
At terminal velocity, net force = 0:
m g = b v t 2 mg = bv_t^2 m g = b v t 2 โ
v t = m g b = ( 5.0 ) ( 9.8 ) 0.25 v_t = \sqrt{\frac{mg}{b}} = \sqrt{\frac{(5.0)(9.8)}{0.25}} v t โ = b m
v t = 196 v_t = \sqrt{196} v t โ = 196 โ
v t = 14 ย m/s \boxed{v_t = 14 \text{ m/s}} v t โ = 14 ย m/s โ
(b) Differential equation:
Newton's second law (taking down as positive):
m d v d t = m g โ b v 2 m\frac{dv}{dt} = mg - bv^2 m d t d v โ = m g โ b v
d v d t = g โ b m v 2 \boxed{\frac{dv}{dt} = g - \frac{b}{m}v^2} d t d v โ = g โ
Or: d v d t = g ( 1 โ v 2 v t 2 ) \frac{dv}{dt} = g\left(1 - \frac{v^2}{v_t^2}\right) d t d v โ = g ( 1 โ
(c) Time to reach 90% of v_t:
d v g ( 1 โ v 2 / v t 2 ) = d t \frac{dv}{g(1 - v^2/v_t^2)} = dt g ( 1 โ v 2 / v t 2 โ )
Using partial fractions or substitution u = v/v_t:
โซ 0 0.9 v t d v g ( 1 โ v 2 / v t 2 ) = โซ 0 t d t \int_0^{0.9v_t} \frac{dv}{g(1 - v^2/v_t^2)} = \int_0^t dt โซ 0 0.9 v t โ โ
Result (hyperbolic tangent):
v t g tanh โก โ 1 ( v v t ) = t \frac{v_t}{g}\tanh^{-1}\left(\frac{v}{v_t}\right) = t g v t โ โ tanh
At v = 0.9v_t:
t = v t g tanh โก โ 1 ( 0.9 ) t = \frac{v_t}{g}\tanh^{-1}(0.9) t = g v t โ โ tanh
t = 14 9.8 tanh โก โ 1 ( 0.9 ) = ( 1.43 ) ( 1.472 ) t = \frac{14}{9.8}\tanh^{-1}(0.9) = (1.43)(1.472) t = 9.8 14 โ tanh โ 1 ( 0.9 ) =
t = 2.1 ย s \boxed{t = 2.1 \text{ s}} t = 2.1 ย s โ
Note: tanh โก โ 1 ( 0.9 ) = 1 2 ln โก ( 1 + 0.9 1 โ 0.9 ) = 1 2 ln โก ( 19 ) = 1.472 \tanh^{-1}(0.9) = \frac{1}{2}\ln\left(\frac{1+0.9}{1-0.9}\right) = \frac{1}{2}\ln(19) = 1.472 tanh โ 1 ( 0.9 ) = 2
โพ
Yes, this page includes 3 practice problems with detailed solutions. Each problem includes a step-by-step explanation to help you understand the approach.
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