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EFFECTS OF DISTRIBUTED ROUGHNESS HEIGHT ON AERODYNAMIC CHARACTERISTICS AND BOUNDARY -LAYER TRANSITION OF A WING-BODY-TALL CONFIGURATION AT A MACH NUMBER OF 1.61

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BookPublisher: Nasa, Washington, D.C. 1964Description: 20.DDC classification: NASA | TN D-2334

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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-2334 (Browse shelf)	Not for loan		TR13614

Total holds: 0

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Previous	NASA TN D-2330 - NUMERICAL SOLUTIONS OF FREE-MOLECULE FLOW IN CONVERGING AND DIVERGING TUBES AND SLOTS	NASA TN D-2332 CONTROL-SURFACE INTERACTION EFFECTS ON DELTA-WING WINDWARD PRESSURES AT A MACH NUMBER OF 6.83 AT HIGH ANGLES OF ATTACK	NASA TN D-2333 A THEORETICAL STUDY OF THE MARTIAN AND THE CYTHERIAN IONOSPHERES	NASA TN D-2334 EFFECTS OF DISTRIBUTED ROUGHNESS HEIGHT ON AERODYNAMIC CHARACTERISTICS AND BOUNDARY -LAYER TRANSITION OF A WING-BODY-TALL CONFIGURATION AT A MACH NUMBER OF 1.61	NASA TN D-2335 EFFECT OF STAGE SPACING ON PERFORMANCE OF 3.75-INCH-MEAN-DIAMETER TWO-STAGE TURBINE HAVING PARTIAL ADMISSION IN THE FIRST STAGE	NASA TN D-2336 PRELIMINARY ANALYSIS OF VARIATION OF PITCH MOTION OF A VEHICLE IN A SPACE ENVIRONMENT DUE TO FUEL SLOSHING IN A RECTANGULAR TANK	NASA TN D-2337 FLIGHT EVALUATION OF THREE TECHNIQUES OF DEMONSTRATING THE MINIMUM FLYING SPEED OF A DELTA-WING AIRPLANE	Next

Bound With Nasa Tn D-2331-2333,2335-2340

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