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EFFECTS OF FOREBODY LENGTH ON THE STABILITY AND CONTROL CHARACTERISTICS AT A MACH NUMBER OF 2.01 OF A CANARD AIRPLANE CONFIGURATION WITH A TRAPEZOIDAL ASPECT-RATIO-3 WING

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BookPublisher: Nasa, Washington, D.C. 1962Description: 30.DDC classification: NASA | TN D-1263

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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-1263 (Browse shelf)	Not for loan		TR13020

Total holds: 0

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Previous	NASA TN D-1250 SUBSONIC WIND-TUNNEL INVESTIGATION OF ERRORS INDICATED BY TOTAL-PRESSURE TUBES IN THE FLOW FIELD OF A BODY SIMULATING THE NOSE OF THE X-15 RESEARCH AIRPLANE	NASA TN D-126 A HIGH-PERFORMANCE 250-POUND-THRUST ROCKET ENGINE UTILIZING GOAXIAL-FLOW INJECTION OF JP-4 FUEL AND LIQUID OXYGEN	NASA TN D-1262 STATISTICAL STUDY OF EFFECTS OF INSERTION ERRORS ON ASCENT TRAJECTORIES FOR LUNAR MISSIONS	NASA TN D-1263 EFFECTS OF FOREBODY LENGTH ON THE STABILITY AND CONTROL CHARACTERISTICS AT A MACH NUMBER OF 2.01 OF A CANARD AIRPLANE CONFIGURATION WITH A TRAPEZOIDAL ASPECT-RATIO-3 WING	NASA TN D-1264 PRESSURE DISTRIBUTIONS AT MACH NUMBER 2.05 ON A SERIES OF HIGHLY SWEPT ARROW WINGS EMPLOYING VARIOUS DEGREES OF TWIST AND CAMBER	NASA TN D-1265 DETERMINATION OF THE CREEP DEFLECTION AND LIFETIME OF ALUMINUM-ALLOY MULTIWEB BOX BEAMS SUBJECTED TO VERIED LOADS AT CONSTANT TEMPERATURE	NASA TN D-1266 INDUCED PRESSURES ON CYLINDRICAL RODS WITH VARIOUS NOSE DRAGS AND NOSE SHAPES AT MACH NUMBERS OF 17 AND 21	Next

Bound With Nasa Tn D-1261-1262,1264-1270

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