Wind tunnel testing
Found in 3 Collections and/or Records:
"Large-Scale Wind-Tunnel Tests on an Aspect Ratio 2.17 Delta-Wing Model Equipped with Midcord Boundary-Layer-Control Flaps" (NASA Technical Note TN D-2552), 1964-12
Document Type: Technical Research Report.
Purpose: Authoritative reference
Authority: Government Civil
Document Number: NASA Technical Note TN D-2552, dated December 1964.
Scope: Preliminary NASA research report by David G. Koenig and Victor R. Corsiglia of Ames Research Center, Moffett Field, Calif.
Contents: See title
"Wind-Tunnel Investigation of a Tilt-Wing VTOL Airplane with Articulated Rotors" (NASA Technical Note TN D-2538), 1965-03
Document Type: Technical Research Report.
Purpose: Authoritative reference
Authority: Government Civil
Document Number: NASA Technical Note TN D-2538, dated March 1965.
Scope: Preliminary NASA research report by James A. Weiberg and Demo J. Giulianetti of Ames Research Center, Moffett Field, Calif.
Contents: See title
"Wind-Tunnel Test of a Full-Scale, 1.1 Pressure Ratio, Ducted Lift-Cruise Fan" (NASA Technical Note TN D-2498), 1964-11
Document Type: Technical Research Report.
Purpose: Authoritative reference
Authority: Government Civil
Document Number: NASA Technical Note TN D-2498, dated November 1964.
Scope: Preliminary NASA research report by Demo J. Giulianetti, James C. Biggers and Victor R. Corsiglia of Ames Research Center, Moffett Field, Calif.
Contents: See title