Subsonic and Transonic Roll Damping Measurements on Basic Finner-Reference-Cited by-同舟云学术

Subsonic and Transonic Roll Damping Measurements on Basic Finner

Published:1982-01 Issue:1 Volume:19 Page:86-87
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Murthy H. Sundara¹

Affiliation:

1. National Aeronautical Laboratory, Bangalore, India

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/3.62210

Reference7 articles.

1. Stability coefficients of a missile at angles of attack

2. On the Pure Rolling Motion of Winged And/Or Finned Missiles in Varying Supersonic Flight

3. ROLL DAMPING MOMENT MEASUREMENTS FOR THE BASIC FINNER AT SUBSONIC AND SUPERSONIC SPEEDS

4. Experimental Missile Pitch- and Moll-Damping Characteristics at Large

5. Sundara Murthy, H., Prasada Rao, K., and Vasudeva, N.S. "Development of a Roll-Damping Test Rig for Measurements on Continuously Rotating Models in the NAL 0.3 m Trisonic Slowdown Tunnel,"NAL Rept. AE-TM-1-81, Jan. 1981.

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