Wind-tunnel sonic-boom testing techniques.-Reference-Cited by-同舟云学术

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Wind-tunnel sonic-boom testing techniques.

Published:1967-05 Issue:3 Volume:4 Page:245-249
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

CARLSON H. W.¹,MORRIS O. A.¹

Affiliation:

1. NASA Langley Research Center, Hampton, Va.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.43827

Reference14 articles.

1. Carlson, H. W. "An investigation of some aspects of the sonic boom by means of wind-tunnel measurements of pressures about several bodies at a Mach number of 2.01," NASA TN D-16K1959).

2. Morris, O. A. "A wind-tunnel investigation at a Mach number of 2.01 of the sonic-boom characteristics of three wing-body combinations differing in wing longitudinal location," NASA TND-1384(1962).

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