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WIND-TUNNEL INVESTIGATION OF HELICOPTER-ROTOR WAKE EFFECTS ON THREE HELICOPTER FUSELAGE MODELS

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BookSeries: NASA Technical Memorandum. Publisher: NASA, Washington, D.C. 1975Description: 205p.Subject(s): Aerodymics

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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-3185	Not for loan		TR10280

Total holds: 0

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Previous	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	NASA TN [D6092]	NASA TN [D-6093]	NASA TN [D-6094]	Next

Technical Memorandum X-3181-90
Bound Vol. No.TR117214; contents:TR10277-10286

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