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SUBSONIC FLIGHT TESTS OF A1/7-SCALE RADIO-CONTROLLED MODEL OF THE NORTH AMERICAN X-15 AIRPLANE WITH PARTICULAR REFERENCE TO HIGH ANGLE -OF -ATTACK CONDTTIONS

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BookPublisher: Nasa,Washington, D.C. 1961Description: 44.DDC classification: NASA | TM X-283

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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 TM X-283 (Browse shelf)	Not for loan		TR13673

Total holds: 0

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Previous	NASA TM X-2641 - ANNOTATED BIBLIOGRAPHY OF PYRRONE AND BBB PUBLICATIONS	NASA TM X-27 - EFFECTS OF OUTBOARD THICKENED AND BLUNTED LEADING EDGES ON THE WAVE DRAG OF A 45[DEGREE] SWEPT-WING AND BODY COMBINATION	NASA TM X-28 - DESIGN ANALYSIS OF A SUBSONIC NUCLEAR-POWERED LOGISTIC AIRPLANE WITH HELIUM-COOLED REACTOR	NASA TM X-283 SUBSONIC FLIGHT TESTS OF A1/7-SCALE RADIO-CONTROLLED MODEL OF THE NORTH AMERICAN X-15 AIRPLANE WITH PARTICULAR REFERENCE TO HIGH ANGLE -OF -ATTACK CONDTTIONS	NASA TM X-288 AN INVESTIGATION AT SUBSONIC SPEEDS OF AERODYNAMIC CHARACTERISTICS AT ANGLES OF ATTACK FROM -4(DEGRE) TO 100(DEGRE) OF A DELTA-WING REENTRY CONFIGURATION HAVING FOLDING WINGTIP PANELS	NASA TM X-289 FIN LOADS AND TIP-CONTROL HINGE MOMENTS ON A1/8-SCALE MODEL SIMULATING THE FIRST STAGE OF THE SCOUT RESEARCH VEHICLE AT A MACH NUMBER OF 2.01	NASA TM X-291 WIND-TUNNEL INVESTIGATION OF STATIC AERODYNAMIC CHARACTERISTICS OF A1/9-SCALE MODEL OF A PROJECT MERCURY CAPSULE AT MACH NUMBERS FROM 1.60 TO 4.65	Next

Bound With Nasa Tm X-281,288-299,Lack No. 282,84-87,90,93,95,96,98

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