Some Numerical Solutions of Inviscid, Unsteady, Transonic Flows over the NLR 7301 Airfoil.
GENERAL DYNAMICS SAN DIEGO CA CONVAIR DIV
Pagination or Media Count:
Inviscid transonic flows over the NLR 7301 airfoil were calculated using a program based on the unsteady Euler equations. The six cases treated include a subsonic flow, a near-shockless supercritical flow and some supercritical flows with shocks. In each case, steady flows and unsteady flows for pitching oscillations with 0.5 degree amplitude and reduced frequency k omega C2U sub infinity of approximately 0.2 were calculated. Author
- Numerical Mathematics
- Computer Programming and Software
- Fluid Mechanics