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THE LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF A RE-ENTRY CONFIGURATION BASED ON A BLUNT 13 DEGREE HALF-CONE AT MACH NUMBERS TO 0.92

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BookPublisher: Nasa, Washington, D.C. 1961Description: 63.DDC classification: NASA | TM X-571

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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-571 (Browse shelf)	Not for loan		TR14314

Total holds: 0

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Previous	NASA TM X-547 WIND-TUNNEL INVESTIGATION AT MACH NUMBERS FROM 0.30 TO OF THE STATIC AERODYNAMIC CHARACTERISTICS OF MODIFIED MERCURY ESCAPE AND EXIT CAPSULE CONFIGURATIONS	NASA TM X-566 SUBSONIC AERODYNAMIC CHARACTERISTICS OF DISK RE-ENTRY CONFIGURATIONS WITH ELLIPTIC CROSS SECTIONS AND THICKNESS-DIAMETER RATIOS OF 0.225 AND 0.325	NASA TM X-569 EFFECTS OF TRANSVERSE CENTER-OF-GRAVITY DISPLACEMENT, AFTERBODY GEOMETRY, AND FRONT-FACE CURVATURE ON THE AERODYNAMIC CHARACTERISTICS OF MERCURY-TYPE MODELS AT A MACH NUMBER OF 5.5	NASA TM X-571 THE LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF A RE-ENTRY CONFIGURATION BASED ON A BLUNT 13 DEGREE HALF-CONE AT MACH NUMBERS TO 0.92	NASA TM X-581 THE SUBSONIC AERODYNAMIC CHARACTERISTICS OF SOME BLUNT DELTA CONFIGURATIONS WITH 75 DEGREE SWEEPBACK	NASA TM X-75 - NASA TM [X-75]	NASA TM X-8 AERODYNAMIC CHARACTERISTICS AT MACH NUMBERS FROM 1.6 TO 2.8 OF 74 (DEGRE) SWEPT ARROW WINGS WITH AND WITHOUT CAMBER AND TWIST	Next

Bound With Nasa Tm X-507-569,581 Lack No.509-13,515-17,519-21,523-29,531-39,541-46,548-65,567-68,572-80

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