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INVESTIGATION AT HIGH SUBSONIC SPEEDS OF THE USE OF LOW AUXILIARY TAIL SURFACES HAVING DIHEDRAL TO IMPROVE THE LONGITUDINAL AND DIRECTIONAL STABILITY OF A T-TAIL MODEL AT HIGH LIFT

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BookPublisher: Nasa, Washington, D.C. 1961Description: 23.DDC classification: NASA | TN D-804

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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-804 (Browse shelf)	Not for loan		TR15838

Total holds: 0

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Previous	NASA TN D-792 - ATTITUDE CONTROL REQIREMENTS FOR HOVERING DETERMINED THROUGH THE USE OF A PILOTED FLIGHT SIMULATOR	NASA TN D-802 A PRELIMINARY INVESTIGATION OF THE EFFECT OF BUMPERS AS A MEANS OF REDUCING PROJECTILE PENETRATION	NASA TN D-803 EFFECTS OF MASS-LOADING VARIATIONS AND APPLIED MOMENTS ON MOTION AND CONTROL OF A MANNED ROTATING SPACE VEHICLE	NASA TN D-804 INVESTIGATION AT HIGH SUBSONIC SPEEDS OF THE USE OF LOW AUXILIARY TAIL SURFACES HAVING DIHEDRAL TO IMPROVE THE LONGITUDINAL AND DIRECTIONAL STABILITY OF A T-TAIL MODEL AT HIGH LIFT	NASA TN D-805 TENSILE AND COMPRESSIVE CREEP OF 6A\|-4V TITANIUM-ALLOY SHEET AND METHODS FOR ESTIMATING THE MINIMUM CREEP RATE	NASA TN D-806 THE BEHAVIOR OF BERYLLIUM AND BERYLLIUM COPPER IN A 4,000(DEGRE) F SUPERSONIC AIR JET AT A MACH NUMBER OF 2	NASA TN D-807 FREE-FLIGHT SKIN-TEMPERATURE AND SURFACE-PRESSURE MEASUREMENTS ON A HIGHLY POLISHED NOSE HAVING A 100 (DEGRE) TOTAL -ANGLE CONE AND A 10 (DEGRE) HALF-ANGLE CONICAL FLARE SECTION UP TO A MACH NUMBER O	Next

Bound With Nasa Tn D-801-803,805-810

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