Wind Tunnel Test of Gurney Flaps and T-Strips on an NACA 23012 Wing
25th, AIAA applied aerodynamics conference ; 2007 ; Miami, FL
2007-01-01
4175 pages
Held on CD-ROM. Papers in range 2007 3800 to 4620 with gaps; Held in e-store (RMS)
Aufsatz (Konferenz)
Englisch
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High-speed wind-tunnel tests of NACA 23012 and 23012-64 airfoils
Engineering Index Backfile | 1941
|Wind-tunnel investigation of NACA 23012 airfoil with 30-percent-chord venetian-blind flaps
Engineering Index Backfile | 1942
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