Preliminary Study on Side-Wall Boundary Layers in Transonic Shock Tube Airfoil Testing
46th, Aerospace sciences meeting AIAA ; 2008 ; Reno, NV
2008-01-01
10 pages
Aufsatz (Konferenz)
Englisch
Aerospace , AIAA , Aeronautics , Astronautics
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PRELIMINARY STUDY ON DIAPHRAGMLESS SHOCK TUBE FOR TRANSONIC AIRFOIL TESTING WITH PDI
British Library Conference Proceedings | 2010
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