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FORCE-TEST INVESTIGATION OF THE STABILITY AND CONTROL CHARACTERISTICS OF A FOUR-PROPELLER TILT-WING VTOL MODEL WITH A PROGRAMED FLAP

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BookPublisher: Nasa, Washington, D.C. 1962Description: 55.DDC classification: NASA | TN D-1389 -

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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-1389 - (Browse shelf)	Not for loan		TR9557

Total holds: 0

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Previous	NASA TN D-1386 - EXPERIMENTAL INVESTIGATION OF THE EFFECTS OF COMPRESSIVE STRESS ON THE FLUTTER OF A CURVED PANEL AND A FLAT PANEL AT SUPERSONIC MACH NUMBERS	NASA TN D-1387 - ATMOSPHERE AS A PART OF THE SPACE ENVIRONMENT	NASA TN D-1388 - DRAG CHARACTERISTICS AND DYNAMIC STABILITY IN DESCENT OF A ROTARY PARACHUTE TESTED IN A VERTICAL TUNNEL	NASA TN D-1389 - FORCE-TEST INVESTIGATION OF THE STABILITY AND CONTROL CHARACTERISTICS OF A FOUR-PROPELLER TILT-WING VTOL MODEL WITH A PROGRAMED FLAP	NASA TN D-1390 - Flight investigation of the longitudinal stability and control characteristics of a four-propeller tilt-wing vtol model with a programed flap	NASA TN D-1402 OPERATIONAL EXPERIENCES AND CHARACTERISTICS OF THE X-15 FLIGHT CONTROL SYSTEM	NASA TN D-1403 THERMODYNAMIC CONSISTENCY OF SOLUBILITY DATA FOR THE HYDROGEN-HELIUM VAPOR-LIQUID SYSTEM	Next

Bound With Nasa Tn D-1381-90

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