Aerodynamics of hypersonic flight at altitudes wherein laws of continuum flow theory apply; expressions for lift, drag, and pitching moment coefficients derived; application to various airfoil sections; airfoil formulas can be applied to finite wings with reasonable accuracy for design estimations.
Two-dimensional airfoils at moderate hypersonic velocities
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 19 , n 9
1952
8 pages
Bibliography
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Two-dimensional airfoils in hypersonic flows
Engineering Index Backfile | 1949
|Oblique Detonation at Hypersonic Velocities
AIAA | 1991
|Heatshield materials erosion at hypersonic velocities
AIAA | 1976
|