Author:
ZHANG Laiping,CHANG Xinghua,MA Rong,ZHAO Zhong,WANG Nianhua
Funder
National Key Research and Development Program
National Natural Science Foundation of China
Subject
Mechanical Engineering,Aerospace Engineering
Reference36 articles.
1. Zuniga FA, Cliff SE, Kinney DJ, Smith SC, Hawke VM, Tang CY. Vehicle design of a sharp CTV concept using a virtual flight rapid integration test environment. Reston: AIAA; 2002. Report No.: AIAA-2002-4881.
2. Lawrence FC, Mills BH. Status update of the AEDC wind tunnel virtual flight testing development program. Reston: AIAA; 2002. Report No.: AIAA-2002-0168.
3. Initial virtual flight test for a dynamically similar aircraft model with control augmentation system;Guo;Chin J Aeronaut,2017
4. Murri DG, Nguyen LT, Grafton SB. Wind tunnel free-flight investigation of a model of a forward swept-wing fighter configuration. Washington, D.C.: NASA; 1984. Report No.: NASA TP-2230.
5. Digital flight: The last CFD aeronautical grand challenge;Salas;J Sci Comput,2006
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