Survey of Blunt-Body Supersonic Dynamic Stability-Reference-Cited by-同舟云学术

Survey of Blunt-Body Supersonic Dynamic Stability

Published:2017-01 Issue:1 Volume:54 Page:109-127
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Kazemba Cole D.¹,Braun Robert D.²,Clark Ian G.³,Schoenenberger Mark⁴

Affiliation:

1. STC, Inc., NASA Ames Research Center, Moffett Field, California 94035

2. Georgia Institute of Technology, Atlanta, Georgia 30332-0150

3. Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California 91109

4. NASA Langley Research Center, Hampton, Virginia 23681–2199

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.A33552

Reference82 articles.

1. AllenJ. H. “Motion of a Ballistic Missile Angularly Misaligned with the Flight Path Upon Entering the Atmosphere and Its Effect Upon Aerodynamic Heating, Aerodynamic Loads, and Miss Distance,” NACA TN-4048, 1957.

2. TobakM.AllenJ. H. “Dynamic Stability of Vehicles Traversing Ascending or Descending Paths Through the Atmosphere,” NACA TN-4275, 1958.

3. BirdJ. D. “Stability of Ballistic Reentry Bodies,” NACA RM L-58, 1958.

4. FletcherH. S. “Damping in Pitch and Static Stability of a Group of Blunt Bodies from M=0.6 to 0.95,” NASA TM X-194, 1959.

5. FletcherH. S.WolhartW. D. “Damping in Pitch and Static Stability of Supersonic Impact Nose Cones, Short Blunt Subsonic Impact Nose Cones, and Manned Reentry Capsules at Mach Numbers from 1.93 to 3.05,” NASA TM X-347, 1960.

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