Experimental Data Base Selected for RTO/AVT Numerical and Analytical Validation and Verification: ONERA 70-deg Delta Wing

Author:

Mitchell Anthony1

Affiliation:

1. U.S. Air Force Academy

Publisher

American Institute of Aeronautics and Astronautics

Reference39 articles.

1. information.15-19

2. -350 -300 -250 -200 -150 -100 -50 -20 0 20 40 60 80 100 120 140 160 180 200 220U/U0 3.4 3.2 3 2.8 2.6 2.4 2.2 2 1.8 1.6 1.4 1.2 1 0.8 0.6 0.4 0.2 0 -0.2

3. Y( mm) -350 -300 -250 -200 -150 -100 -50 -20 0 20 40 60 80 100 120 140 160 180 200 220U/U0 3.4 3.2 3 2.8 2.6 2.4 2.2 2 1.8 1.6 1.4 1.2 1 0.8 0.6 0.4 0.2 0 -0.2

4. Y( mm ) -350 -300 -250 -200 -150 -100 -50 -20 0 20 40 60 80 100 120 140 160 180 200 220U/U0 3.4 3.2 3 2.8 2.6 2.4 2.2 2 1.8 1.6 1.4 1.2 1 0.8 0.6 0.4 0.2 0 -0.2

5. Y( mm) -350 -300 -250 -200 -150 -100 -50 -20 0 20 40 60 80 100 120 140 160 180 200 220

Cited by 4 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. A Reduced-Complexity Investigation of Blunt Leading-Edge Separation Motivated by UCAV Aerodynamics (Invited);53rd AIAA Aerospace Sciences Meeting;2015-01-03

2. Mach Number Effects on Vortex Breakdown in Subsonic Flow over a Delta Wing;49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2011-01-04

3. Comparison of DES and URANS for Unsteady Vortical Flows over Delta Wings;45th AIAA Aerospace Sciences Meeting and Exhibit;2007-01-08

4. NATO RTO AVT Task Group-080 "Vortex Breakdown over Slender Wings": Objectives and Overview;21st AIAA Applied Aerodynamics Conference;2003-06-21

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