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EXPERIMENTAL PERFORMANCE OF A CONTROL PRESSURE PROBE AT MACH NUMBERS OF 3.0,4.5, AND 6.0.

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BookPublisher: Nasa, Washington, D.C. 1966Description: 20.DDC classification: NASA | TN D-3719

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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-3719 (Browse shelf)	Not for loan Untraceable		TR15628

Total holds: 0

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Previous	NASA TN D-3716 BAFFLE THICKNESS EFFCTS IN FUEL SLOSHING EXPRERIMNTS.	NASA TN D-3717 THE NEAR-EARTH METEROID ENVIORNMENT	NASA TN D-3718 SUBSONIC LONGITUDINAL AERODYNAMIC CHRACTERISTICS OF A 40 DEGREE SEMIAPEX ANGLE CONICAL REENTRY CONFIGURATION.	NASA TN D-3719 EXPERIMENTAL PERFORMANCE OF A CONTROL PRESSURE PROBE AT MACH NUMBERS OF 3.0,4.5, AND 6.0.	NASA TN D-372 A FLIGHT STUDY OF THE CONVERSION MANEUVER OF A TILT-DUCT VTOL AIRCRAFT	NASA TN D-3720 STELLAR EVOLUTION 1 CALIBRATION OF THE HERZSPRUNG-RUSSELL DIAGRAM IN TERMS OF AGE AND MASS FOR MAIN-SEQUENCE B AND A STARS.	NASA TN D-3722 BINARY DIFFUSION IN AN EXPONENTIAL MEDIUM	Next

Bound With Nasa Tn D-3712-3718,3720.

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