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MPARATIVE EVULATION OF THODS FOR PREDICATING UTTER AND DIVERGENCE OF SWEPT WINGS OF FINITE SPAN.

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BookPublisher: Nasa, Washington, D.C. 1963Description: 53.DDC classification: NASA | TN D-2051

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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-2051 (Browse shelf)	Not for loan		65593

Total holds: 0

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Previous	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-2051 MPARATIVE EVULATION OF THODS FOR PREDICATING UTTER AND DIVERGENCE OF SWEPT WINGS OF FINITE SPAN.	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.	NASA TN D-2055 STUDY OF THE USE OF TERMINAL CONTROL TECHNIQUES FOR GUIDENCE DURING DIRECT AND SKIP ENTRIES FOR A CAPSULE-TYPE VEHICLE AT PARABOLIC VELOCITY.	Next

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