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33 Cards in this Set

  • Front
  • Back
Cyl e-r
cos(T) i + sin(T) j
Cyl e-theta
-sin(T) i + cos(T) j
e-tang
cos(P)i+sin(P)j
e-norm
-sin(P)i+cos(P)j
Sph e-r
sin(P)cos(T)i + sin(P)sin(T)j + cos(P)k
Sph e-phi
cos(P)cos(T)i+cos(P)sin(T)j-sin(P)k
Sph e-theta
-sin(T)+cos(T)j
Primative Variables
(Definition)
Variables which can be explained but not defined
Primative Variables (4)
Space, Time, Mass, Force
Defined Variables(3)
Position, Velocity, Acceleration
Axioms Definition
Statements based on observations, not proofs. These are based on variables.
Newton's 1st law/axiom
In an inertial dreference frame, if the sum of forces acting on a particle (∑F) is zero, the particle is at rest, or in a state of uniform velocity.
Note: Inertial reference frame- a box on the floor isn’t technically “moving” even though the earth is spinning. It all depends on how you define your “frame”.
Newton's 2nd law/axiom
In an inertial reference, frame, if the sum of forces acting on a particle is not zero (∑F≠0), the sum of the forces (∑F) is proportional to the time rate of change of momentum (mv ⃗_P ) of the particle
Note: Integrate mv and you get m∙a (force) (F=ma)
Newton's 3rd law/axiom
3. In an inertial reference frame, the interaction between any two (2) particles is through a pair of forces equal in magnitude, opposite in direction, and act along the straight long joining the two (2) particles.
Note: For every action, there is an equal and opposite reaction.
K
constant in newton's 2nd law which takes into account variation in units
Steps to solving a problem
1. Define a Coord system
2. In motion diagram
3. FBD
w (omega)
sqrt(k/m)
Use this equation to help solve for homogeneous linear equations
x=Ae^lamba(t)
Sph X
rsin(P)cos(T)
Sph Y
rsin(P)sin(T)
Sph Z
rcos(P)
System of Particle Applications
1. Rigid Body Dynamics
2. Deformable Body Dynamics
3. Fluid Dynamics
4. Fluids
5. Control
6. Combustion
Potential Energy
U=mgh
Kinetic Energy
K=1/2 mv^2
Spring Force
kx
Centripetal Force
(mv^2)/R
Radius of Curvature
P
Curvature
d(T)/ds
Cyl Vp
R(dot) e-r + r(thetadot) e-theta + zdot k
Cyl Ap
[R(dbldot)-r(thetadot)^2]e-r + [2(rdot)thetadot+r(thetadbldot)] e-theta + zdbldot k
Tan Vp
sdot(e-t)
Tan Ap
sdbldot(e-t)+((sdot)^2)/p (e-n)
sphr Vp
rdot (e-r) +r(thetadot)sin(P) (e-theta) + r(phidot)(e-phi)