Experimental-theoretical correlation of supersonic jet-on base pressure for cylindrical afterbodies-Reference-Cited by-同舟云学术

Experimental-theoretical correlation of supersonic jet-on base pressure for cylindrical afterbodies

Published:1970-09 Issue:5 Volume:7 Page:474-477
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

ADDY A. L.¹

Affiliation:

1. University of Illinois at Urbana-Champaign, Urbana, III.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.44201

Reference22 articles.

1. Addy, A. L. "Analysis of the Axisymmetric Base-Pressure and Base-Temperature Problem with Supersonic Interacting Freestream-Nozzle Flows Based on the Flow Model of Korst et al., Part II: A Comparison and Correlation with Experiment for Cylindrical Afterbodies/' Rept. RD-TR-69-13, Dec. 1969, U.S. Army Missile Command, Redstone Arsenal, Ala.

2. Carriere, P. and Sirieix, M. "Resultats Re*cents dans 1'Etude des Problemes de Melange et de Recollement," T.P. No. 165, Office National d'Etudes et de Recherches Aerospatiales (ONERA), 29, 1964, Avenue de la Division Leclerc, Chatillonsous-Bagneux (Seine), France; also Library Translation No. 1113, May 1965, Royal Aircraft Establishment, Ministry of Aviation, Farnborough, Hants, England.

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