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WING AND FLAP LOADS OBTAINED FROM A WIND-TUNNEL INVESTIGATION OF A LARGE-SCALE V/STOL MODEL

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BookPublisher: Nasa, Washington, D.C. 1963Description: 89.DDC classification: NASA | TN D-1634

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	NASA TN D-1634 (Browse shelf)	Not for loan		TR15019

Total holds: 0

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Previous	NASA TN D-1630 OFF-DESIGN AERODYNAMIC CHRACTERISTICS AT MACH NUMBERS 1.61 AND 2.20 OF A SERIES OF HIGHLY SWEPT ARROW WINGS DESIGNED FOR MACH NUMBER 2.0 EMPLOYING VARIOUS DEGREES OF TWIST AND CAMBER.	NASA TN D-1632 AN EXTENSION OF ESTIMATED HYPERSONIC FLOW PARAMETERS FOR HELIUM AS A REAL GAS	NASA TN D-1633 INVESTIGATION OF BUFFET PRESSURES ON MODELS OF LARGE MANNED LAUNCH VEHICLE CONFIGURATIONS	NASA TN D-1634 WING AND FLAP LOADS OBTAINED FROM A WIND-TUNNEL INVESTIGATION OF A LARGE-SCALE V/STOL MODEL	NASA TN D-1635 AN EXPERIMENTAL STUDY OF THE BEHAVIOR OF SPHERES ABLATING UNDER CONSTANT AERODYNAMIC CONDITIONS	NASA TN D-1636 A THEORETICAL STUDY OF THE MOTION OF AN IDEALIZED PLASMA RING THROUGH VARIOUS TRAVELING-MAGNETIC-WAVE PLASMA ACCELERATIONS	NASA TN D-1637 QUALITATIVE EVALUATION OF EFFECT OF HELICOPTER ROTOR-BLADE TIP VORTEX ON BLADE AIRLOADS	Next

Bound With Nasa Tn D-1631-33,1635-40

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