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QUALITATIVE EVALUATION OF EFFECT OF HELICOPTER ROTOR-BLADE TIP VORTEX ON BLADE AIRLOADS

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BookPublisher: Nasa, Washington, D.C. 1963Description: 46.DDC classification: NASA | TN D-1637

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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-1637 (Browse shelf)	Not for loan		TR15022

Total holds: 0

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Previous	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	NASA TN D-1638 LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF SEVERAL FIFTH-STAGE SCOUT REENTRY VEHICLES FROM MACH NUMBER 0.60 TO 24.4 INCLUDING SOME REYNOLDS NUMBER EFFECTS ON STABILITY AT HYPERSONIC SPEEDS	NASA TN D-1639 ORBITAL ERROR ANALYSIS OF THE SCOUT RESEARCH VEHICLE	NASA TN D-1640 MEASUREMENTS OF FLOW ANGLES IN VICINITY OF TWO LIFTING FOREBODY CONFIGURATIONS AT A MACH NUMBER OF 2.01	Next

Bound With Nasa Tn D-1631-36,1638-40

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