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METHOD FOR PREDICTING SHOCK SHAPES AND PRESSURE DISTRIBUTIONS ON TWO-DIMENSIONAL AIRFOILS AT LARGE ANGLES OF ATTACK

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BookPublisher: Nasa, Washington, D.C. 1973Description: V,45.DDC classification: NASA | TN D-7197 -

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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-7197 - (Browse shelf)	Not for loan		TR9272

Total holds: 0

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Previous	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	NASA TN D-720 EFFECT OF RATIO OF JET AREA TO TOTAL AREA AND OF PRESSURE RATIO ON LIFT AUGMENTATION OF ANNULAR JETS IN GROUND EFFECT UNDER STATIC CONDITIONS	Next

Bound With Nasa Tn D-7190-99

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