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PRESSURE MEASUREMENT ON TWO 60 DEGREE SWEPT DELTA WINGS WITH BLUNT LEADING EDGES AND DIHEDRAL ANGLES OF 0 DEGREE AND 45 DEGREE AT A MACH NUMBER OF 4.95

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BookPublisher: Nasa, Washington, D.C. 1962Description: 24.DDC classification: NASA | TN D-1246

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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-1246 (Browse shelf)	Not for loan		TR12805

Total holds: 0

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Previous	NASA TN D-1243 DESIGN OF THE NASA LIGHTWEIGHT INFLATABLE SATELLITES FOR THE DETERMINATION OF ATMOSPHERIC DENSITY AT EXTREME ALTITUDES	NASA TN D-1244 A TABULATION OF SECTION AERODYNAMIC CHARACTERISTICS AT MACH NUMBERS OF 1.61 AND 2.01 FOR FOUR SWEPT WINGS HAVING THE SAME PLANFORM BUT DIFFERENT SURFACE SHAPES	NASA TN D-1245 LOW-SPEED AERODYNAMIC CHARACTERISTICS OF A CANARD AIRPLANE CONFIGURATION HAVING SPLIT FLAPS LOCATED AHEAD OF THE WING TRAILING EDGE AND LEADING-AND TRAILING -EDGE FLAPS ON THE CANARD CONTROL	NASA TN D-1246 PRESSURE MEASUREMENT ON TWO 60 DEGREE SWEPT DELTA WINGS WITH BLUNT LEADING EDGES AND DIHEDRAL ANGLES OF 0 DEGREE AND 45 DEGREE AT A MACH NUMBER OF 4.95	NASA TN D-1247 A MATRIX METHOD FOR THE DETERMINATION OF THE NATURAL VIBRATIONS OF FREE-FREE UNSYMMETRICAL BEAMS WITH APPLICATION TO LAUNCH VEHICLES	NASA TN D-1248 THE METEORITIC HAZARD OF THE ENVIRONMENT OF A SATELLITE	NASA TN D-1249 STATISTICAL WIND DISTRIBUTION DATA FOR USE AT NASA WALLOPS STATION	Next

Bound With Nasa Tn D-1241-45, 1247-50

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