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NASA TN [D-1050] : estimate of shock standoff distance ahead of a general stagnation point

By: Reshotko, Eli.

Series: NASA Technical Note. D-1050.Publisher: NASA, Washington, D.C. 1961Description: 19p.Subject(s): Aerodynamics

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Item type	Current location	Collection	Call number	Vol info	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)		NASA TN D-1050	Not for loan		TR8636

Total holds: 0

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Previous	EXPERIMENTAL INVESTIGATION OF AN AIR-COOLED TURBINE OPERATING IN A TURBOJET ENGINE AT TURBINE INLET TEMPERATURES UP TO 2500(DEGREE)	NASA TN [D-1047]	ANNULAR INTERNAL-EXTERNAL-EXPANSION ROCKET NOZZLES FOR LARGE BOOSTER APPLICATIONS	NASA TN [D-1050]	NASA Technical Note: PLANETARY PROBE GUIDANCE ACCURACY INFLUENCE FACTORS FOR CONJUNCTION-CLASS MISSIONS	NASA Technical Note: USE OF BARONTI-LIBBY TRANSFORMATION AND PRESTON TUBE CALIBRATIONS TO DETERMINE SKIN FRICTION FROM TURBULENT VELOCITY PROFILES	Applicability of mixing length thory to a turbulent vortex system [NASA TN D-1051]	Next

Technical Note D-1041-50
Bound Vol. No.65506; Contents: TR8629-36

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