A new semiempirical method for computing nonlinear angle-of-attack aerodynamics on wing-body-tail configurations-Reference-Cited by-同舟云学术

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A new semiempirical method for computing nonlinear angle-of-attack aerodynamics on wing-body-tail configurations

Published:1993-01-11 Issue: Volume: Page:
ISSN:
Container-title:31st Aerospace Sciences Meeting
language:
Short-container-title:

Author:

MOORE F.¹,DEVAN L.¹,HYMER T.¹

Affiliation:

1. U.S. Navy, Naval Surface Warfare Center, Dahlgren, VA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1993-34

Reference28 articles.

1. Devan, L.,and Mason,I.Aerodynamicsof Tactical WeaponstoMachNumber 8andAngle ofAttack 180': Part II,ComputerProgramand UsersGuide,NSWC TR 81-358,Dahlgren,VA, Sep 81. Devan, L.,Mason,L.,andMoore,F.G."Aerodynamics ofTacticalWeaponstoMach Numher 8andAngle ofAttack 180","AIAAPaper 82-0250. Moore, F.G.,BodyAloneAerodynamics of Guidedand UnguidedProjectiles atSubsonic, Transonicand SupersonicMach Numbers, NWL TR-2796Dahlgren, VA,Nov 1972.

2. Van Dyke, M. D."First-andSecond-Order Theory ofSupersonic Flow Past BodiesofRevolution,"JAS,Mar 1951.

3. ' & 7, DeJarnette, F.R.,Ford,C.P.,andYoung, D.E. "ANewMethod forCalculatingSurfacePressuresonBodies atanAngle ofAttack inSupersonicFlow,"AIAAPaper 79-1552,Jul 1974.

Cited by 1 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. An improved version of the Naval Surface Warfare Center aeroprediction code (AP93);Journal of Spacecraft and Rockets;1994-09

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