Fluctuating Pressure Environment of a Drag Reduction Spike-Reference-Cited by-同舟云学术

Fluctuating Pressure Environment of a Drag Reduction Spike

Published:1977-12 Issue:12 Volume:14 Page:705-710
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Guenther Rolf A.¹,Reding J. Peter¹

Affiliation:

1. Lockheed Missiles & Space Company, Inc., Sunnyvale, Calif.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/3.57253

Reference8 articles.

1. French, N.J. and Jecmen, D.M. "Transonic/Supersonic Wind Tunnel Investigation of Effects of Parametric Variations in Nose Fairing and Aerospike Geometry on Trident I C4 Missile Body Static Stability and Drag (C4A-1, E-78), (C4A-C41, E-79)," Lockheed Missiles and Space Co., TM 81-11/77, LMSC/D366908, 1974.

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