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XB-70 COMPRESSURE-NOISE REDUCTION AND PROPULSION-SYSTEM PERFORMANCE FOR CHOKED INLET FLOW

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BookPublisher: Nasa, Washington, D.C. 1970Description: 25.DDC classification: NASA | TN D-5692

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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-5692 (Browse shelf)	Not for loan		TR12104

Total holds: 0

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Previous	NASA TN D-5687 EFFECT OF WALL ROUGHNESS ON THE DAMPING OF LIQUID OSCILLATIONS IN RECTANGULAR TANKS	NASA TN D-5688 PRELIMINARY TESTS OF A SIMPLIFIED MODULAR TURBOJET COMBUSTOR	NASA TN D-5689 EFFECT OF SULFUR, OXYGEN,AND HYDROGEN SULFIDE SURFACE FILMS ON THE ADHESION OF CLEAN IRON	NASA TN D-5692 XB-70 COMPRESSURE-NOISE REDUCTION AND PROPULSION-SYSTEM PERFORMANCE FOR CHOKED INLET FLOW	NASA TN D-5693 X-RAY OBSERVATIONS OF FLOW PATTERNS IN A MERCURY BOILER	NASA TN D-5694 HEAT TRANSFER AND LEVITATION OF A SPHERE IN LEIDENFROST BOILING	NASA TN D-5695 WIND-TUNNEL INVESTIGATION OF A V/STOL TRANSPORT MODEL WITH SIX WING-MOUNTED LIFT FANS	Next

Bound With Nasa Tn D-5690, 5693-5699 Lack No. 5691.

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