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Fluid flow analysis of a hot-core hypersonic-wind-tunnel nozzle concept [NASA TN D-6768]

By: Anders, John B.

Contributor(s): Sebacher, Daniel I | Boatright, William B.

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BookSeries: National Aeronautics and Space Administration [NASA]. Publisher: Washington, D.C. National Aeronautics and Space Administration [NASA] 1972Description: 24p.Subject(s): Fluid flow analysisDDC classification: NASA | TN D-6768

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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-6768 (Browse shelf)	Not for loan		TR015806

Total holds: 0

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Previous	NASA TN D-6765 Arched-outer-race ball-bearing analysis considering centrifugal forces [TN D-6765]	NASA TN D-6766 Fortran program for generating a two-dimensional orthogonal mesh between two arbitrary boundaries [TN D-6766]	NASA TN D-6767 Parametric analysis of performance and design characteristics for advanced earth-to-orbit shuttles [NASA TN D-6767]	NASA TN D-6768 Fluid flow analysis of a hot-core hypersonic-wind-tunnel nozzle concept [NASA TN D-6768]	NASA TN D-6769 Influence of silicon on friction and wear of iron-cobalt alloys [NASA TN D-6769]	NASA TN D-6840 OPTICAL ABSORPTION IN FUSED SILICA AT ELEVATED TEMPERATURES DURING 1.5-MEV ELECTRON IRRADIATION.	NASA TN D-685 AN EXPLICIT LINEAR FILTERING SOLUTION FOR THE OPTIMIZATION OF GUIDANCE SYSTEMS WITH STATISTICAL INPUTS	Next

Bound with NASA TN D-6760-6769

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