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A FLIGHT INVESTIGATION OF AN AUTOMATIC GUST-ALLEVIATION SYSTEM IN A TRANSPORT AIRPLANE.

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BookPublisher: Nasa, Washington, D.C. 1961Description: 91.DDC classification: NASA | TN D-532

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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-532 (Browse shelf)	Not for loan		TR16045

Total holds: 0

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Previous	NASA TN D-5316 - SUBSONIC AERODYNAMIC CHARACTERISTICS OF A LARGE-SCALE 1.075-PRESSURE-RATIO TIP-TURBINE CRUISE-FAN PROPULSION SYSTEM AT ANGLE OF ATTACK	NASA TN D-5318 - EFFECT OF FLUID TEMPERATURE ON THE CAVITATION PERFORMANCE OF A HIGH HUB-TIP RATIO AXIAL FLOW PUMP IN WATER TO 250(DEGREE) F (394 K)	NASA TN D-5319 - ENERGY TRANSFER AND ION COST IN A HYDROGEN PLASMA	NASA TN D-532 A FLIGHT INVESTIGATION OF AN AUTOMATIC GUST-ALLEVIATION SYSTEM IN A TRANSPORT AIRPLANE.	NASA TN D-5320 - FABRICATION PROCESS FOR GLASS COATED ELECTRON-BOMBARDMENT ION THRUSTER GRIDS	NASA TN D-5322 - STUDY OF HELIUM PENETRATION AND SPREDING IN A MACH 2 AIRSTREAM USING A DELTA WING INJECTOR	NASA TN D-5323 - TESTS OF SODIUM BOILING IN A SINGLE TUBE-IN-SHELL HEAT EXCHANGER OVER THE RANGE 1720(DEGREE) TO 1980(DEGREE) F (1211 TO 1355 K)	Next

Bound With Nasa Tn D- 531,533-540.

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