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LONGITUDINAL TRIM CHARACTERISTICS OF A DEFLECTED SLIPSTREAM V/STOL AIRCRAFT DURING LEVEL FLIGHT AT TRANSITION FLIGHT SPEEDS

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BookPublisher: Nasa, Washington, D.C. 1962Description: 19.DDC classification: NASA | TN D-1430

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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-1430 (Browse shelf)	Not for loan		TR14857

Total holds: 0

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Previous	NASA TN D-1427 ATMOSPHERE ENTRIES WITH SPACECRAFT LIFT-DRAG RATIOS MODULATED TO LIMIT DECELERATIONS	NASA TN D-1428 A 1-FOOT HYPERVELOCITY SHOCK TUNNEL IN WHICH HIGH-ENTHALPY,REAL-GAS AIR FLOWS CAN BE GENERATED WITH FLOW TIMES OF ABOUT 180 MILLISECONDS	NASA TN D-1429 THERMODYNAMIC AND TRANSPORT PROPERTY CORRELATION FORMULAS FOR EQUILIBRIUM AIR FROM 1,000(DEGRE) K TO 15,000(DEGRE ) K	NASA TN D-1430 LONGITUDINAL TRIM CHARACTERISTICS OF A DEFLECTED SLIPSTREAM V/STOL AIRCRAFT DURING LEVEL FLIGHT AT TRANSITION FLIGHT SPEEDS	NASA TN D-1432 - LARGE SCALE WIND-TUNNEL TESTS OF A CIRCULAR PLAN-FORM AIRCRAFT WITH A PERIPHERAL JET FOR LIFT, THRUST, AND CONTROL	NASA TN D-1433 - ANALYSIS OF GUIDANCE PERTURBATION FOR A LOW-THURST MARS ORBITER MISSION USING SNAP-8	NASA TN D-1435 - HEAT-TRANSFER CHARACTERISTICS OF SEVERAL RADIATOR FINNED-TUBE CONFIGURATIONS	Next

Bound With Nasa Tn D-1421-1429

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