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Measurments of aerodynamic heat transfer and boundary- layer transition on A 10 deg con in free flight at supersonic mach numbers up to 5.9

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BookPublisher: Washington D. C. National Aeronautics and Space Administration (NASA) 1961Description: 33p.Subject(s): Fluid Mechanics and ThermodynamicsDDC classification: NASA | TN D-745

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)	NASA TN D-745 (Browse shelf)	Not for loan		TR11868

Total holds: 0

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Previous	NASA TN D-743 Aerodynamic intraction effects ahead of a sonic jet exhausting perpendiculary from a flat plate in to a mach number 6 free stream	NASA TN D-744 Airspeed operating practices of turbine-powered commercial transport airplanes	NASA TN D-7440 APOLLO EXPERIENCE REPORT COMMAND MODULE CREW-COUCH/RESTRAINT AND LOAD-ATTENUATION SYSTEMS	NASA TN D-745 Measurments of aerodynamic heat transfer and boundary- layer transition on A 10 deg con in free flight at supersonic mach numbers up to 5.9	NASA TN D-746 Flight Controllability limits and related human transfer functions as determined from simulator and flight tests	NASA TN D-747 ANALOG SIMULATION OF A PILOT-CONTROLLED RENDEZVOUS.	NASA TN D-748 ANALYSIS OF A FOUR-STATION DOPPLER TRACKING METHOD USING A SIMPLE CW BEACON.	Next

Bound With NASA TN D-741-750

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