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NASA Technical Note [NASA TN D-2550]: Application of generalized Newtonian theory to three-dimensional sharp-nose shock-detached bodies at mach for angles of attack up to 25 [degree]

By: Washington. National Aeronautics and Space Administration (NASA).
Contributor(s): Ashby, George C | Goldberg, Theodore J.
Material type: materialTypeLabelBookSeries: National Aeronautics and Space Administration ; NASA Technical Note. Publisher: Washington NASA 1965Description: 41p.Subject(s): Aerodynamics | Newtonian theory | Hypersonic flow
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Bound together NASA TN D-2541 to 2550

Bound vol. Acc. No. 67642 contains Acc. No. TR9902 to TR9910

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