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Weak incident shock interactions with mach 8 laminar boundary layers [NASA TN D -7835]

By: Kaufman,Louis G.

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BookSeries: National Aeronaitics and Space Adminstration ; NASA Technical Note. Publisher: Wahington.D. C. National Aeronaitics and Space Adminstration 1974Description: 45p.Subject(s): Laminar boundary layers

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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 7831-7835	Not for loan		TR002573

Total holds: 0

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Previous	Selection and preliminary evaluation of three structures as potential solid conductors of alkali ions: Two hollandities a titanate and a tungstate [NASA TN D-7157]	A fortan program for determining aircraft stability and control derivatives from flight data [NASA TN D -7831]	25- Mb sounding data and synoptic charts for NASA's ave ii pilot experiment[NASA TN D-7832]	Weak incident shock interactions with mach 8 laminar boundary layers [NASA TN D -7835]	Comparison of three methods for calculation of helicopter rotor blade loading and stresses due to stall [NASA TN D-7833]	Application of parameter identification technique to a hingeless helicopter rotor[NASA TN D -7834]	Pressure distributions on two-dimensional sharp-leading-edge flat plates with sweep angles of 0 degree,30 degree,and 45 degree at a mach number of 6 and angles of attack from 0 degree to 90 degree[NASA TN D-1371]	Next

Bound vol. contains D 7831- 7835

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