A Philosophy for Improved Rocket Nozzle Design-Reference-Cited by-同舟云学术

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A Philosophy for Improved Rocket Nozzle Design

Published:1957-10 Issue:10 Volume:27 Page:1088-1093
ISSN:1936-9980
Container-title:Journal of Jet Propulsion
language:en
Short-container-title:Journal of Jet Propulsion

Author:

DILLAWAY ROBERT B.¹

Affiliation:

1. Rocketdyne, A Division of North American Aviation, Canoga Park, Calif.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Reference22 articles.

1. Isenberg, J. S., and Lin, C. C , "The Method of Characteristics in Compressible Flow," P a r t I, Steady Supersonic Flow, Technical Intelligence-Air Materiel Command, Technical Report F-TR-1173A-ND (GDAM A-9-M 11/1) Monograph II, 1947.

2. Ibid, Part la, Tables and Charts, Technical Report F-TR1173B-ND (GDAM A-9-M 11/A).

Cited by 7 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Rocket nozzles: 75 years of research and development;Sādhanā;2021-04-11

2. Design of a double parabolic supersonic nozzle and performance evaluation by experimental and numerical methods;Aircraft Engineering and Aerospace Technology;2018-01-07

3. GEOMETRICAL CONSTRUCTION OF TWO-DIMENSIONAL AND AXISYMMETRICAL FLOW FIELDS;AIAA Journal;1963-10

4. Recent Developments in Rocket Nozzle Configurations;ARS Journal;1961-11

5. Contour Nozzles;ARS Journal;1960-03

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