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A SIMULATOR STUDY TO DETERMINE PILOT OPINION OF THE TRIM CHANGES WITH POWER FOR DEFLECTED SLIPSTREAM STOL AIRPLANES

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BookPublisher: Nasa, Washington, D.C. 1966Description: 33.DDC classification: NASA | TN D-3246

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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-3246 (Browse shelf)	Not for loan		TR13515

Total holds: 0

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Previous	NASA TN D-323 A FLIGHT STUDY OF A POWER- OFF LANDING TECHNIQUE APPLICABLE TO RE-ENTRY VEHICLES	NASA TN D-3230 AN EXPERIMENTAL INVESTIGATION OF HEAT TRANSFER TO TURBULENT FLOW IN SMOOTH TUBES FOR THE REACTING N2O-NO2 STSTEM.	NASA TN D-324 THE DESIGN OF FEEDBACK CONTROL SYSTEMS CONTAINING A SATURATION TYPE NONLINEARITY	NASA TN D-3246 A SIMULATOR STUDY TO DETERMINE PILOT OPINION OF THE TRIM CHANGES WITH POWER FOR DEFLECTED SLIPSTREAM STOL AIRPLANES	NASA TN D-3252 FRACTURE MECHANICS OF THROUGH-CRACKED CYLINDRICAL PRESSURE VESSELS	NASA TN D-3253 EXPERIMENTAL PRESSURE DROP INVESTIGATION OF WETTING AND NONWETTING MERCURY CONDENSING IN UNIFORMLY TAPERED TUBES	NASA TN D-3254 THEORETICAL ELASTIC MISMATCH STRESSES	Next

Bound With Nasa Tn D-3241-45,3247-50

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