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FREE-FLIGHT INVESTIGATION AT MACH NUMBERS BETWEEN 0.5 AND 1.7 OF THE ZERO-LIFT ROLLING EFFECTIVENESS AND DRAG OF VARIOUS SURFACE, SPOILER, AND JET CONTROLS ON AN 80(DEGRE) DELTA-WING MISSILE

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BookPublisher: Nasa, Washington, D.C. 1960Description: 47.DDC classification: NASA | TN D-205

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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-205 (Browse shelf)	Not for loan		TR14834

Total holds: 0

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Previous	NASA TN D-2047 EFFECTS OF DIFFERENTIAL PRESSURE, THARMAL STRESS, AND BUCKLING ON FLUTTER OF FLAT PANELS WITH LENGHT-WIDTH RATIO OF 2	NASA TN D-2048 BOUNDARY-LAYER VELOCITY PROFILES AND SKIN FRICTION DUE TO SURFACE ROUGHNESS ON AN OGIVE CYLINDER AT MACH NUMBERS OF 1.61 AND 2.01	NASA TN D-2049 FEASIBILITY STUDY OF A BANG-BANG PATH CONTROL FOR A REENTRY VEHICLE.	NASA TN D-205 FREE-FLIGHT INVESTIGATION AT MACH NUMBERS BETWEEN 0.5 AND 1.7 OF THE ZERO-LIFT ROLLING EFFECTIVENESS AND DRAG OF VARIOUS SURFACE, SPOILER, AND JET CONTROLS ON AN 80(DEGRE) DELTA-WING MISSILE	NASA TN D-2050 EFFECTS OF FLANK LOSSES IN THE THEORY OF SPACE-PROBE ENTRY UNDER CONDITIONS OF HIGH MASS LOSS.	NASA TN D-2052 THE DESIGN OF SAILPLANES FOR OPTIMUM THERMAL SOARING PERFORMANCE.	NASA TN D-2053 WIND-COMPENSATION METHOD AND RESULTS OF ITS APPLICATION TO FLIGHT TESTS OF TWELVE TRILBLAZER ROCKET VEHICLES.	Next

Bound With Nasa Tn D-201-204,206-210

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