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Flight-Test investigation of ailerons as a source of yaw control on the VZ-2 tilt-wing aircraft : TN D-1375

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BookPublisher: Washington NASA 1962Description: 24p.Subject(s): Aircraft -- VZ-2 tilt-wing | AileronsDDC classification: TRNASATND-1375

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Item type	Current location	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	TRNASATND-1375 (Browse shelf)	Not for loan		TR7449

Total holds: 0

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Previous	TRNASATND-1372 Heat-Transfer and Pressure Measurements on a flat-plate surface and heat-transfer measurements on attached protuberances in a supersonic turbulent boundary layer at mach numbers of 2.65, 3.51, and 4.44	TRNASATND-1373 Use of conformal mapping to determine the apparent additional mass of scalloped and/or clustered cylinder configurations with experimental evaluations of results	TRNASATND-1374 Low-Speed longitudinal aerodynamic characteristics associated with a series of low-aspect-ratio wings having variations in leading-edge contour	TRNASATND-1375 Flight-Test investigation of ailerons as a source of yaw control on the VZ-2 tilt-wing aircraft	TRNASATND-4832 Calculated and flight-measured handling-qualitiies factors of three subsonic Jet transports	TRNASATND-4833 Mechanical properties and column behavior of thin-wall beryllium tubing	TRNASATND-4835 Influence of angle of glide slope on the accuracy of performing instrument approaches in a simulator	Next

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