Computational Evaluations of Experimental Data for Sonic Boom Models with Nozzle Jet Flow Interactions-Reference-Cited by-同舟云学术

Computational Evaluations of Experimental Data for Sonic Boom Models with Nozzle Jet Flow Interactions

Published:2017-01-05 Issue: Volume: Page:
ISSN:
Container-title:55th AIAA Aerospace Sciences Meeting
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Author:

Jensen James C.¹,Denison Marie¹,Durston Don²,Cliff Susan E.²

Affiliation:

1. Science and Technology Corporation

2. NASA Ames Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2017-0042

Reference29 articles.

1. Experimental Validations of a Low Boom Aircraft Design

2. 5Magee, Todd E., Fugal, Spencer R., Fink, Lawrence E., Adamson, Eric E., and Shaw, Stephen G. "System-Level Experimental Validations for Supersonic Commercial Transport Aircraft Entering Service in the 2018-2020 Time Period, Phase II Final Report," NASA CR (to be published).

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