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A RESTRAINT SYSTEM ENABLING PILOT CONTROL UNDER MODERTELY HIGH ACCEKERATION IN A VARIED ACCELERATION FIELD .

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BookPublisher: Nasa, Washington, D.C. 1960Description: 19.DDC classification: NASA | TN D-91

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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-91 (Browse shelf)	Not for loan		63634

Total holds: 0

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Previous	NASA TN D-907 - LOCAL AERODYNAMIC HEAT TRANSFER AND BOUNDARY-LAYER TRANSITION ON ROUGHENED SPHERE-ELLIPSOID BODIES AT MACH NUMBER 3.0	NASA TN D-908 - DEVELOPMENT OF AN 8-INCH BY 8-INCH SLOTTED TUNNEL FOR MACH NUMBERS UP TO 1.28	NASA TN D-909 - ANALYTICAL INVESTIGATION OF AN ADAPTIVE FLIGHT-CONTROL SYSTEM USING A SINUSOIDAL TEST SIGNAL	NASA TN D-91 A RESTRAINT SYSTEM ENABLING PILOT CONTROL UNDER MODERTELY HIGH ACCEKERATION IN A VARIED ACCELERATION FIELD .	NASA TN D-910 - MAGNETIC IGNITION OF PULSED GAS DISCHARGES IN AIR OF LOW PRESSURE IN A COAXIAL PLASMA GUN	NASA TN D-92 MEASURED AND THEORETICAL FLOW FIELDS BEHIND A RETANGULAR AND A TRIANGULAR WING UP TO HIGH ANGLES OF AATACK AT A MACH NUMBER OF 2.46.	NASA TN D-922 - REPEATABILITY, DRIFT, AND AFTEREFFECT OF THREE TYPES OF AIRCRAFT ALTIMETERS	Next

Bound With Nasa Tn D-92-100.

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