Influence of airplane configuration on sonic- boom characteristics-Reference-Cited by-同舟云学术

Influence of airplane configuration on sonic- boom characteristics

Published:1964-03 Issue:2 Volume:1 Page:82-86
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

CARLSON HARRY W.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/10.2514/3.43562

Reference11 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-161(1959).

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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