Aerodynamic Design and Analysis of High Performance Nozzles for Mach 4 Accelerator Vehicles-Reference-Cited by-同舟云学术

Aerodynamic Design and Analysis of High Performance Nozzles for Mach 4 Accelerator Vehicles

Published:2006-01-09 Issue: Volume: Page:
ISSN:
Container-title:44th AIAA Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Georgiadis Nicholas¹,DalBello Teryn¹,Trefny Charles¹,Johns Albert¹

Affiliation:

1. NASA Glenn Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-16

Reference13 articles.

1. Shafer, D.G.and McNelis, N.B. "Development of a Ground Based Mach 4+ Revolutionary TurbineAccelerator Technology Demonstrator (RTATD) for Access to Space,"ISOABEPaper 2003-1125,2003.

2. Hagemann,G., Immich,H., and Terhardt, M. "Flow Phenomena in Advanced RocketNozzles - ThePlug Nozzle,"AIAA Paper 98-3522,July 1998.

3. Plug Nozzle Flowfield Analysis

4. Hagemann,G., Schwane, R., Reijasse, P.,and Ruf, J. "NASA RTO WG 10: CFD Results of Plug Nozzle Test Cases,"AIAA Paper 2002-4036,July 2002.

5. Nelson, C.C. and Power, G.D. "CHSSI Project CFD-7: The NPARC AllianceFlow Simulation System,"AIAA Paper 2001-0594,Jan. 2001.

Cited by 5 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. Study of a Plug Nozzle for Supersonic Aircraft Concepts;30th AIAA/CEAS Aeroacoustics Conference (2024);2024-05-30

2. Flow and noise from supersonic plug nozzles;28th AIAA/CEAS Aeroacoustics 2022 Conference;2022-06-13

3. A study of flow and noise from supersonic plug nozzles;AIAA AVIATION 2021 FORUM;2021-07-28

4. A numerical simulation study of the path-resolved breakup behaviors of molten metal in high-pressure gas atomization: With emphasis on the role of shock waves in the gas/molten metal interaction;Advanced Powder Technology;2018-03

5. An Overview of the NPARC Alliance's Wind-US Flow Solver;48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition;2010-01-04