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EFFECT OF SKEWED WING-TIP CONTROLS ON A VARIABLE-SWEEP WING-FUSELAGE CONFIGURATION

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BookPublisher: Nasa, Washington, D.C. 1967Description: 93.DDC classification: NASA | TN D-3847

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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-3847 (Browse shelf)	Not for loan Untraceable		TR13051

Total holds: 0

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Previous	NASA TN D-3844 MATRIX ANALYSIS OF LONGITUDINAL AND TORSIONAL VIBRATIONS IN NONUNIFORM MULTIBRANCH BEAMS	NASA TN D-3845 ROLLING STABILITY DERIVATIVES OF A VARIABLE-SWEEP TACTICAL FIGHTER MODEL AT SUBSONIC AND TRANSONIC SPEEDS	NASA TN D-3846 A NUMERICAL METHOD FOR DETERMINING HEATING RATES FROM THICK-CALORIMETER DATA	NASA TN D-3847 EFFECT OF SKEWED WING-TIP CONTROLS ON A VARIABLE-SWEEP WING-FUSELAGE CONFIGURATION	NASA TN D-3848 A THREE-DIMENSIONAL ANALYSIS OF A TANGENTIAL YO-YO DESPIN DEVICE ON A ROTATING BODY	NASA TN D-3849 MECHANISM OF CADMIUM SULFIDE FILM CELL	NASA TN D-3850 PREDICTIONS OF SHOCK-LAYER RADIATION FROM MOLECULAR BAND SYSTEMS IN PROPOSED PLANETARY ATMOSPHERES	Next

Bound With Nasa Tn D-3841-3846,3848-3850

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