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EXPERIMENTAL INVESTIGATION OF COMPRESSOR STALL USING AN ON-LINE DISTORTION INDICATOR AND SIGNAL CONDITIONER

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BookSeries: NASA Technical Memorandum.Publisher: NASA, Washington, D.C. 1975Description: 31p.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 TM X-3182	Not for loan		TR10277

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Previous	Satellite view of typhoon marie 1966 development [NASA TN D-4757]	Anomalous diffusion in a plasma formed from the exhaust beam of an electron-bombardment ion thruster [NASA, TN D-4758]	Noncavitating and cavitating performance of two low-area-ratio water jet pumps with throat lengths of 5.66 diameters [Nasa TN D-4759]	EXPERIMENTAL INVESTIGATION OF COMPRESSOR STALL USING AN ON-LINE DISTORTION INDICATOR AND SIGNAL CONDITIONER	AERODYNAMIC ANALYSIS OF SEVERAL HIGH THROAT MACH NUMBER INLETS FOR THE QUIET CLEAN SHORT-HAUL EXPERIMENTAL ENGINE	DIGITAL COMPUTER STUDY OF NUCLEAR REACTOR THERMAL TRANSIENTS DURING STARTUP OF 60-K WE BRAYTON POWER CONVERSION SYSTEM	WIND-TUNNEL INVESTIGATION OF HELICOPTER-ROTOR WAKE EFFECTS ON THREE HELICOPTER FUSELAGE MODELS	Next

Technical Memorandum X-3181-90
Bound Vol. No.117214; contents:TR10277-10286

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