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STUDY OF FLOW OVER OSCILLATING AIRFOIL MODELS AT A MACH NUMBER OF 7.0 IN HELIUM

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BookPublisher: Nasa, Washington, D.C. 1961Description: 21.DDC classification: NASA | TN D-992

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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-992 (Browse shelf)	Not for loan		TR15881

Total holds: 0

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Previous	NASA TN D-988 - FREE FLIGHT INVESTIGATION OF HEAT TRANSFER TO AN UNSWEPT CYLINDER SUBJECTED TO AN INCIDENT SHOCK AND FLOW INTERFERENCE FROM AN UPSTREAM BODY AT MACH NUMBERS UP TO 5.50	NASA TN D-989 - SUMMARY OF FLIGHT-TEST RESULTS OF THE VZ-2 TILT WING AIRCRAFT	NASA TN D-990 - METHODS FOR DETERMINING THE OPTIMUM DESIGN OF STRUCTURES PROTECTED FROM AERODYNAMIC HEATING AND APPLICATION TO TYPICAL BOOST-GLIDE OR REENTRY FLIGHT PATHS	NASA TN D-992 STUDY OF FLOW OVER OSCILLATING AIRFOIL MODELS AT A MACH NUMBER OF 7.0 IN HELIUM	NASA TN D-993 STATIC LONGITUDINAL STABILITY OF A ROCKET VEHICLE HAVING A REAR-FACING STEP AHEAD OF THE STABILIZING FINS	NASA TN D-994 AERODYNAMIC CHARACTERISTICS OF TOWED CONES USED AS DECELERATORS AT MACH NUMBERS FROM 1.57 TO 4.65	NASA TN D-995 AERODYNAMIC LOADS ON AN ISOLATED SHROUDED-PROPELLER CONFIGURATION FOR ANGLES OF ATTACK FROM- 10 (DEGREE) TO 110 (DEGREE)	Next

Bound With Nasa Tn D-991,993-1000

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