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COMPARISON OF THE AERODYNAMIC CHARACTERISTICS OF AN ABLATING AND NONABLATING BLUNTED CONICAL BODY

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BookPublisher: Nasa, Washington, D.C. 1973Description: IV,22.DDC classification: NASA | TN D-7196 -

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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-7196 - (Browse shelf)	Not for loan		TR9271

Total holds: 0

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Previous	NASA TN D-7193 - APPLICATION OF PHASE-CHANGE TECHNIQUE TO THIN SECTIONS WITH HEATING ON BOTH SURFACES	NASA TN D-7194 - WIND-TUNNEL INVESTIGATION OF EFFECTS OF VARIATIONS IN REYNOLDS NUMBER AND LEADING-EDGE TREATMENT ON THE AERODYNAMIC CHARACTERISTICS OF AN EXTERNALLY BLOWN JET-FLAP CONFIGURATION	NASA TN D-7195 - CALCULATION OF ENERGY DEPOSITION DISTRIBUTIONS FOR SIMPLE GEOMETRIES	NASA TN D-7196 - COMPARISON OF THE AERODYNAMIC CHARACTERISTICS OF AN ABLATING AND NONABLATING BLUNTED CONICAL BODY	NASA TN D-7197 - METHOD FOR PREDICTING SHOCK SHAPES AND PRESSURE DISTRIBUTIONS ON TWO-DIMENSIONAL AIRFOILS AT LARGE ANGLES OF ATTACK	NASA TN D-7198 - EXPERIMENTAL TEST RESULTS OF A GENERALIZED-PARAMETER FUEL CONTROL	NASA TN D-7199 - AERODYNAMIC EFFECTS OF FIVE LIFT-FAN POD ARRANGEMENTS ON AN UNPOWERED V/STOL TRANSPORT MODEL	Next

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