Critical assessment of the linear plug nozzle concept-Reference-Cited by-同舟云学术

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Critical assessment of the linear plug nozzle concept

Published:2001-07-08 Issue: Volume: Page:
ISSN:
Container-title:37th Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

Hagemann Gerald¹,Immich Hans¹,Dumnov Gennady²

Affiliation:

1. Astrium GmbH, Munich, Germany

2. NIITP, Keldysh Research Center, Moscow, Russia

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2001-3683

Reference23 articles.

1. 5, Sept.Oct. 1998.

2. Press Releases on X-33 Programme Status, Space News, Issues 1998 - 2001.

3. Angelino, G. "Theoretical and Experimental Investigations of the Design and Performance of a Plug Type Nozzle,"NASA TN-12, July 1963.

4. Lee,C.C."Fortran Programs for Plug Nozzle Design,"NASATN R-41, March 1963.

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1. Design and Evaluation of Aerospike Nozzles for an Upper-Stage Application;Journal of Spacecraft and Rockets;2024-07

2. Viscous Wake Effects on the Inviscid Wall-Bounded Jet Flow over an Aerospike Nozzle;AIAA SCITECH 2023 Forum;2023-01-19

3. Study on Control of Unsteadiness and Flow Asymmetry in Linear Aerospike Nozzles;Journal of Spacecraft and Rockets;2023-01

4. Developing and applying Mach 4.5 nozzle in hypersonic wind tunnel;Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University;2021-10

5. Interaction of external flow with linear cluster plug nozzle jet;Shock Waves;2018-07-13

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