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STUDY OF A CONTROL SYSTEM TO ALLEVIATE AIRCRAFT RESPONSE TO HORIZONTAL AND VERTICAL GUSTS

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BookPublisher: Nasa, Washington, D.C. 1973Description: 38.DDC classification: NASA | TN D-7278 -

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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-7278 - (Browse shelf)	Not for loan		TR9647

Total holds: 0

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Previous	NASA TN D-7275 - LOADING AND HEATING OF A LARGE FLAT PLATE AT MACH 7 IN THE LANGLEY 8-FOOT HIGH-TEMPERATURE STRUCTURES TUNNEL	NASA TN D-7276 - EVALUATION OF CONTROL LAWS AND ACTUATOR LOCATIONS FOR CONTROL SYSTEM APPLICABLE TO DEFORMABLE ASTRONOMICAL TELESCOPE MIRRORS	NASA TN D-7277 - ACOUSTIC IMPEDANCE OF CURVED MULTILAYERED DUCT LINERS	NASA TN D-7278 - STUDY OF A CONTROL SYSTEM TO ALLEVIATE AIRCRAFT RESPONSE TO HORIZONTAL AND VERTICAL GUSTS	NASA TN D-7279 - CONTROL AND PROTECTION SYSTEM FOR PARALLELED MODULAR STATIC INVERTER-CONVERTER SYSTEMS	NASA TN D-7281 - Development of the weld-braze	NASA TN D-7282 - Aerodynamic and flow-visalization studies of two delta-wing entry vehicles at a mach number	Next

Bound With Nasa Tn D-7270-79

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