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DEVELOPEMENT OF AN ANALYSIS FOR THE DETERMINATION OF COUPLED HELICOPTER ROTOR /CONTROL SYSTEM RESPONSE,

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BookPublisher: Nasa, Washington, D.C. 1975Description: 112,I.DDC classification: NASA | CR-2452 -

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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 CR-2452 - (Browse shelf)	Not for loan		TR7560

Total holds: 0

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Previous	NASA CR-2449 - FLUCTUATING SURFACE-PRESSURE CHARACTERISTICS ON SLENDER CONES IN SUBSONIC, SUPERSONIC, AND HYPERSONIC MACH-NUMBER FLOW	NASA CR-2450 - A WIND MODEL FOR AN ELEVATED STOL-PORT CONFIGURATION	NASA CR-2451 - DEVELOPEMENT AND APPLICATION OF A NON-GAUSSIAN ATMOSPHERIC TURBULENCE MODEL FOR USE IN FLIGHT SIMULATORS"	NASA CR-2452 - DEVELOPEMENT OF AN ANALYSIS FOR THE DETERMINATION OF COUPLED HELICOPTER ROTOR /CONTROL SYSTEM RESPONSE,	NASA CR-2460 A SYSTEM TO GEOMETRICALLY RECTIFY AND MAP AIRBORNE SCANNER IMAGERY AND TO ESTIMATE GROUND AREA	NASA CR-2461 CAPACITANCE DISCHARGE SYSTEM FOR IGNITION OF SINGLE BRIDGE APOLLO STANDARD INITIATORS (SBASI)	NASA CR-2462 ANALYSIS OF DYNAMIC STALL USING UNSTEADY BOUNDARY-LAYER THEORY	Next

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