Numerical Investigations of the Base-Flow Characteristics of Axisymmetric Aerospike Nozzles-Reference-Cited by-同舟云学术

Numerical Investigations of the Base-Flow Characteristics of Axisymmetric Aerospike Nozzles

Published:2002 Issue:148 Volume:45 Page:108-115
ISSN:0549-3811
Container-title:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:en
Short-container-title:Trans. Japan Soc. Aero. S Sci.

Author:

Ito Takashi¹,Fujii Kozo²

Affiliation:

1. Department of Aeronautics and Astronautics, The University of Tokyo

2. The Institute of Space and Astronautical Science Japan

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://www.jstage.jst.go.jp/article/tjsass/45/148/45_148_108/_pdf

Reference16 articles.

1. 1) Ito, T., Fujii, K. and Hayashi, A. K.: Computations of the Axisymmetric Plug Nozzle Flow Fields, J. Propul. Power, 18 (2002), pp. 254–260, See also AIAA Paper 99-3211.

2. 2) Tomita, T., Tamura, H. and Takahashi, M.: An Experimental Evaluation of Plug Nozzle Flow Fields, AIAA Paper 96-2632, 1996.

3. 3) Ito, T. and Fujii, K.: Flow Field Analysis of the Base Region of Axisymmetric Aerospike Nozzles, AIAA Paper 2001-1051, 2001.

4. 4) Hagemann, G., Immich, H. and Terhardt, M.: Flow Phenomena in Advanced Rocket Nozzles—The Plug Nozzle, AIAA Paper 98-3522, 1998.

5. 5) Immich, H. and Caporicci, M.: Status of the FESTIP Rocket Propulsion Technology Program, AIAA Paper 97-3311, 1997.

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