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A FLIGHT STUDY OF THE DYNAMIC STABILITY OF A TILTING-ROTOR CONVERTIPLANE

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BookPublisher: Nasa, Washington, D.C. 1961DDC classification: NASA | TN D-778

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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-778 (Browse shelf)	Not for loan		TR7489

Total holds: 0

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Previous	NASA TN D-7757 TRANSPORT DYNAMICS OF A HIGH-POWER-DENSITY MATRIX-TYPE HYDROGEN-OXYGEN FUEL CELL	NASA TN D776 AWIND-TUNNEL INVESTIGATION OF A 4-FOOT-DIAMETER DUCTED FAN MOUNTED ON THE TIP OF A SEMISPAN WING	NASA TN D-777 BALLISTIC RANGE MEASUREMENTS OF STAGNATION-POINT HEAT TRANSFER IN AIR IN CARBON DIOXIDE AT VELOCTTIES UP TO 18, 000 FEET PER SECOND	NASA TN D-778 A FLIGHT STUDY OF THE DYNAMIC STABILITY OF A TILTING-ROTOR CONVERTIPLANE	NASA TN D-779 FLIGHT INVESTIGATION USING VARIABLE-STABLITY AIRPLANES OF MINIMUM STABILITY REQUIREMENTS FOR HIGH-SPEED, HIGH-ALTITUDE VEHICLES	NASA TN D-780 A METHODS FOR OBTAINING THE NONLINEAR AERODYNAMIC STABILITY CHARACTERISTICS OF BODIES OF REVOLUTION FROM FREE-FLIGHT TESTS	NASA TN D-792 - ATTITUDE CONTROL REQIREMENTS FOR HOVERING DETERMINED THROUGH THE USE OF A PILOTED FLIGHT SIMULATOR	Next

Bound With Nasa Tn D-771-777, And Tn D-779-80

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