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A STUDY OF BOUNDARY LAYER TRANSITION ON OUTGASSING CONES IN HYPERSONIC FLOW [NASA CR-1908]

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BookSeries: Natioanl Aeronautics and Space Administration(NASA). Publisher: Washington, D.C. NASA 1971Description: ix, 71p.Subject(s): Boundary layer transition | Gas injectionDDC classification: NASA | CR-1908

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	Reference	NASA CR-1908 (Browse shelf)	Not for loan		TR7504

Total holds: 0

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Previous	NASA CR-1902 ATTITUDE-REFERENCED RADIOMETER STUDY- Part II- primary calibration System [NASA CR-1902]	`NASA CR-1905 IMPROVED NEUTRON ACTIVATION PREDICTION CODE SYSTEM DEVELOPMENT [NASA CR-1905]	NASA CR-1907 SNAP-8 ELECTRICAL GENERATING SYSTEM DEVELOPMENT PROGRAM [NASA CR-1907]	NASA CR-1908 A STUDY OF BOUNDARY LAYER TRANSITION ON OUTGASSING CONES IN HYPERSONIC FLOW [NASA CR-1908]	NASA CR-1911 Development and application of a method for predicting rotor free wake positions and resulting rotor blade air loads Volume I [NASA CR-1911]	NASA CR-1912 DEVELOPMENT AND APPLICATION OF A METHOD FOR PREDICTING ROTOR FREE WAKE POSITIONS AND RESULTING ROTOR BLADE AIR LOADS Volume II [NASA CR-1912)	NASA CR-1913 ANALYSIS OF FLIGHT DATA ON BOUNDARY LAYER TRANSITION AT HIGH ANGLES OF ATTACK[NASA CR 1913]	Next

Bound With Nasa Cr-1901-1908(Bound With Acc No.101558)

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