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THE ROLLING MOMENT DUE TO SIDESLIP OF SWEPT WINGS AT SUBSONIC AND TRANSONIC SPEEDS

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BookPublisher: Nasa, Washington, D.C. 1960Description: 81.DDC classification: NASA | TN D-209

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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-209 (Browse shelf)	Not for loan		TR14838

Total holds: 0

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Previous	NASA TN D-207 HYDRODYNAMIC IMPACT-LOADS INVESTIGATION OF CHINE-IMMERSED 0(DEGRE) DEAD-RISE CONFIGURATIONS HAVING LONGITUDINAL CURVATURE WITH AN APPENDED BIBLIOGRAPHY OF LANGLEY IMPACT BASIN HYDRODYNAMIC PUBLICATION	NASA TN D-2070 A NUMBERICAL ANALYSIS OF DIRECT NUCLEAR ELECTROGENERATOR CELLS THAT USE CERIUM 144 BETA-EMITTING RADIOISOTOPE SOURCES	NASA TN D-208 AN INVESTIGATION OF NONPROPAGATING FATIGUE CRACKS	NASA TN D-209 THE ROLLING MOMENT DUE TO SIDESLIP OF SWEPT WINGS AT SUBSONIC AND TRANSONIC SPEEDS	NASA TN D-210 ROTATING-BEAM FATIGUE TESTS OF NOTCHED AND UNNOTCHED 7075-T6 ALUMINUM-ALLOY SPECIMENS UNDER STRESSES OF CONSTANT AND VARYING AMPLITUDES	NASA TN D-2102 ANALYTICAL INVESTIGATION OF REDUCTION IN TURBULENT SKIN FRICTION ON A FLAT PLATE BY MEANS OF AIR INJECTION THROUGH DISCRETE SLOTS	NASA TN D-2103 THE DRIFT OF A 24-HOUR EQUATORIAL SATELLITE DUE TO AN EARTH GRAVITY FIELD THROUGH 4TH ORDER	Next

Bound With Nasa Tn D-201-208,210

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