Experimental Investigation Of A Hypersonic Glider Configuration At A Mach Number Of 6 And At Full Scale Reynolds Numbers
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Index to NASA Technical Publications
| Author | : United States. National Aeronautics and Space Administration |
| Publisher | : |
| Total Pages | : |
| Release | : 1960-07 |
| Genre | : |
| ISBN | : |
Technical Abstract Bulletin
| Author | : Defense Documentation Center (U.S.) |
| Publisher | : |
| Total Pages | : 1116 |
| Release | : 1961-02 |
| Genre | : Technology |
| ISBN | : |
Index of N A S A Technical Publications
| Author | : United States. National Aeronautics and Space Administration |
| Publisher | : |
| Total Pages | : 448 |
| Release | : 1960 |
| Genre | : |
| ISBN | : |
Transition of the Laminar Boundary Layer on a Delta Wing with 74 Degree Sweep in Free Flight at Mach Numbers from 2.8 to 5.3
| Author | : Gary T. Chapman |
| Publisher | : |
| Total Pages | : 46 |
| Release | : 1961 |
| Genre | : Fluid mechanics |
| ISBN | : |
Effects of Angle of Attack and Bluntness on the Hypersonic Flow Over a 15 ̊semiapex Cone in Helium
| Author | : Joseph W. Cleary |
| Publisher | : |
| Total Pages | : 52 |
| Release | : 1970 |
| Genre | : Angle of attack (Aerodynamics) |
| ISBN | : |
Free-flight Measurements of the Static and Dynamic Stability and Drag of a 10 Degree Blunted Cone at Mach Numbers 3.5 and 8.5
| Author | : Peter F. Intrieri |
| Publisher | : |
| Total Pages | : 40 |
| Release | : 1962 |
| Genre | : Noses (Space vehicles) |
| ISBN | : |
