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PRESSURE DISTRIBUTION ON TWO MODELS OF A PROJECT MERCURY CAPSULE FOR A MACH NUMBER RANGE OF 1.60 TO 6.01 AND AN ANGLE-OF-ATTACK RANGE OF 0 DEGREE TO 180 DEGREE

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BookPublisher: Nasa, Washington, D.C. 1960Description: 96.DDC classification: NASA | TM X-336

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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-336 (Browse shelf)	Not for loan		TR16069

Total holds: 0

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Previous	NASA TM X-317 WIND-TUNNEL INVESTIGATION AT MACH NUMBERS FROM 0.40 TO 1.20 OF THE STATIC AERODYNAMIC AND CONTROL CHARACTERISTICS OF A MODEL OF A NONLIFTING REENTRY CAPSULE IN COMBINATION WITH A ROCKET BOOSTER	NASA TM X-33 - ELEVATED-TEMPERATURE TESTS UNDER STATIC AND AERODYNAMIC CONDITIONS ON HONEYCOMBCORE SANDWICH PANELS	NASA TM X-332 AERODYNAMIC CHARACTERISTICS AT MACH NUMBER 2.05 OF A SERIES OF HIGHLY SWEPT ARROW WINGS EMPLOYING VARIOUS DEGREES OF TWIST AND CAMBER	NASA TM X-336 PRESSURE DISTRIBUTION ON TWO MODELS OF A PROJECT MERCURY CAPSULE FOR A MACH NUMBER RANGE OF 1.60 TO 6.01 AND AN ANGLE-OF-ATTACK RANGE OF 0 DEGREE TO 180 DEGREE	NASA TM X-338 SOME AERODYNAMIC AND CONTROL STUDIES OF LIFTING REENTRY COFIGURATIONS AT ANGLES OF ATTACK UP TO 90 DEGREE AT A MACH NUMBER OF 2.91	NASA TM X-34 - ELEVATED-TEMPERATURE TESTS UNDER STATIC AND AERODYNAMIC CONDITIONS ON CORRUGATED-STIFFENED PANELS	NASA TM X-344 BASIC PRESSURE MEASUREMENTS ON A 0.0667-SCALE MODEL OF THE NORTH AMERICAN X-15 RESEARCH AIRPLANE AT TRANSONIC SPEEDS	Next

Bound With Nasa Tm X-300-334,338-45 Lack No.301-04,306-12,315-16,318-31,333,335,337,339-43

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