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STATIC STABILITY CHARACTERISTICS OF THREE THICK WING MODELS WITH PARABOLIC PLAN FORMS AT A MACH NUMBER OF 3.11

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BookPublisher: Nasa, Washington, D.C. 1959Description: 18.DDC classification: NASA | TM X-141

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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-141 (Browse shelf)	Not for loan		TR16232

Total holds: 0

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Previous	NASA TM X-136 TRANSONIC FLUTTER CHARACTERISTICS OF AN ASPECT-RATIO-4, 45(DEGRE) SWEPTBACK, TAPER-RATIO-0.2 PLAN FORM	NASA TM X-137 FLIGHT BEHAVIOR OF THE X-2 RESEARCH AIRPLANE TO A MACH NUMBER OF 3.20 AND A GEOMETRIC ALTITUDE OF 126,200 FEET	NASA TM X-138 EFFECTS OF TWIST AND CAMBER AND THICKNESS ON THE AERODYNAMIC CHARACTERISTICS OF A75 (DEGRE) SWEPT ARROW WING AT A MACH NUMBER OF 2.91	NASA TM X-141 STATIC STABILITY CHARACTERISTICS OF THREE THICK WING MODELS WITH PARABOLIC PLAN FORMS AT A MACH NUMBER OF 3.11	NASA TM X-144 LOW-SPEED MEASUREMENTS OF OSCILLATORY LATERAL STABILITY DERIVATIVES OF A 1/7-SCALE MODEL OF THE NORTH AMERICAN X-15 AIRPLANE	NASA TM X-147 FRICTION AND PRESSURE DRAG OF BOUNDARY-LAYER DIVERTER SYSTEMS AT MACH NUMBER OF 3.0	NASA TM X-149 FERFORMANCE SUMMARY AND ANALYSIS OF A MACH 3.0 DESIGN AXISYMMETRIC ALL-EXTERNAL -COMPRESSION DOUBLE-CONE INLET FROM MACH NUMBER 3.0 TO 0.8	Next

Bound With Nasa Tm X-130-138,144-156,Lack No. 131-34,39-40,42-43,45-46,48-50,52-53,55

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