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EFFECT OF SCREEN-INDUCED TOTAL-PRESSURE DISTORTION ON AXIAL-FLOW COMPRESSOR STABILITY

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BookPublisher: Nasa, Washington, D.C. 1974Description: 78.DDC classification: NASA | TM X-3017 -

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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 TM X-3017 - (Browse shelf)	Not for loan		TR7562

Total holds: 0

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Previous	NASA TM X-3008 - FLIGHT INVESTIGATION OF THE VER AND IFR LANDING APPROACH CHARACTERISTICS AND TERMINAL AREA AIRSPACE REQUIREMENTS FOR A LIGHT STOL AIRPLANE	NASA TM X-3009 - WIND-TUNNEL INVESTIGATION OF AN EXTERNALLY BLOWN FLAP STOL TRANSPORT MODEL INCLUDING AN INVESTIGATION OF WALL EFFECTS	NASA TM X-3010 - SUMMARY OF THE RECENT SHORT-HAUL SYSTEMS STUDIES	NASA TM X-3017 - EFFECT OF SCREEN-INDUCED TOTAL-PRESSURE DISTORTION ON AXIAL-FLOW COMPRESSOR STABILITY	NASA TM X-3025 - MODIFICATION OF A THREE-DIMENSIONAL SUPERSONIC NOZZLE ANALYSIS AND COMPARISON WITH EXPERIMENT DATA	NASA TM X-3029 - CROSSFLOW EFFECTS ON IMPINGEMENT COOLING OF A TURBINE VANE	NASA TM X-3046 - MEASUREMENT OF GASEOUS EMISSIONS FROM A TURBOFAN ENGINE AT SIMULATED ALTITUDE CONDITIONS	Next

Bound With Nasa Tm X-3006-46

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