Hypersonic flow over a yawed circular cone
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in .pdf document. A 10[degree] semi-apex, circular cone is tested in air at Mach 8 and at yaw angles to 24[degrees]; surface pressure, heat transfer, and pitot-pressure throughout the flow field are p...
Similar Items
-
Numerical Investigations of Transition in Hypersonic Flows over Circular Cones
by: Husmeier, Frank
Published: (2008) -
Hypersonic flow over an elliptic cone : theory and experiment
by: Chapkis, Robert L.
Published: (1959) -
Computation and Stability Analysis of Laminar Flow over a Blunt Cone in Hypersonic Flow
by: Esfahanian, Vahid
Published: (1991) -
Computation and stability analysis of laminar flow over a blunt cone in hypersonic flow /
by: Esfahanian, Vahid
Published: (1991) -
Wall pressure beneath a transitional hypersonic boundary layer over an inclined straight circular cone
by: Siwei Dong, et al.
Published: (2020-12-01)