Show how the differential form of the (mathrm{x})-component momentum equation [Equation (2.70a)] can be expressed using the
Question:
Show how the differential form of the \(\mathrm{x}\)-component momentum equation [Equation (2.70a)] can be expressed using the substantial derivative:
\[ \frac{\partial(ho u)}{\partial t}+abla \circ(ho u \boldsymbol{V})=-\frac{\partial p}{\partial x}+ho f_{x}+\left(F_{x}\right)_{v i s c o u s} \]
Next, show how your result above can be generalized for the full momentum conservation equation (in differential form):
\[ \frac{\partial(ho \boldsymbol{V})}{\partial t}+abla \circ(ho \boldsymbol{V} \boldsymbol{V})=-abla p+ho \boldsymbol{f}+\boldsymbol{F}_{\text {viscous }} \]
Fantastic news! We've Found the answer you've been seeking!
Step by Step Answer:
Related Book For
Fundamentals Of Aerodynamics ISE
ISBN: 9781266076442
7th Edition
Authors: John D. Anderson, Jr, Christopher P Cadou
Question Posted: