"भौतिकी के सूत्र" (अनुभाग) सम्पादित करें

== अन्य ==
{| class="wikitable"
|-
|[[inertial frame]]s
|<math>x_{PA} = x_{PB} + x_{AB}</math>
|-
| . . .
|<math>v_{PA} = v_{PB} + v_{AB}</math>
|-
| . . .
|<math>a_{PA} = a_{PB} + 0</math>
|-
|[[trajectory]]
|<math>y=x\tan\theta-gx^2/2(V_0\cos\theta)^2</math>
|-
|flight distance
|<math>v_0^2\sin{2\theta}/g</math>
|-
|[[tension (physics)|tension]], lies within the cord
|<math>f_t = f</math>
|-
|[[mechanical energy]]
|<math> E_{mec}=K + U</math>
|-
|[[mechanical energy]] is conserved
|<math> \Delta E_{mec} = 0</math> when all forces are conservative
|-
|[[thrust]]
|<math>t = Rv_{rel}=ma</math>
|-
|[[ideal rocket equation]]
|<math>\Delta v = ln(m_i/m_f)v_{rel}</math>
|-
|[[parallel axis theorem]]
|<math>I = I_{com} + mr^2</math>
|-
|[[list of moments of inertia]]
|
|-
|[[indeterminate system]]s
|
|}