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FLOW FIELD SURVEY AND DECELERATOR DRAG CHARACTERISTICS IN THE WAKE OF A MODEL OF THE X-15 AIRPLANE AT MACH 2.0 AND 4.65

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BookPublisher: Nasa, Washington, D.C. 1966Description: 35.DDC classification: NASA | TN D-3285 -

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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-3285 - (Browse shelf)	Not for loan		TR10034

Total holds: 0

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Previous	NASA TN D-3282 - EFFECT OF NOSE-MOUNTED CONTROL-SYSTEM JETS IN ROLL-CONTROL POSITIONS ON THE AERODYNAMICS OF A SPACE VEHICLE	NASA TN D-3283 - EMPIRICAL METHOD FOR DETERMINING STATIC DISTRIBUTED AERODYNAMIC LOADS ON AXISYMMETRIC MULTISTAGE LAUNCH VEHICLES	NASA TN D-3284 - EFFECT OF NACELLE ORIENTATION OF THE AERODYNAMIC CHARACTERISTICS OF AN ARROW WING-BOLY CONFIGURATION AT MACH NUMBER 2.03	NASA TN D-3285 - FLOW FIELD SURVEY AND DECELERATOR DRAG CHARACTERISTICS IN THE WAKE OF A MODEL OF THE X-15 AIRPLANE AT MACH 2.0 AND 4.65	NASA TN D-3286 - STUDY OF COAXIAL HALL CURRENT ACCLERATORS AT MODERATE PRESSURES	NASA TN D-3287 - ESTIMATE OF THE CHEMICAL KINETICS BEHIND NORMAL SHOCK WAVES IN MIXTURES OF CARBON DIOXIDE AND NITROGEN FOR CONDITIONS TYPICAL OF MARS ENTRY	NASA TN D-3288 - ZERO- AND REDUCED-GRAVITY SIMULATION ON A MAGNETIC-COLLOID POOL-BOILING SYSTEM	Next

Bound With Nasa Tn D-3281-90

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