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AN IMPROVED METHOD FOR THE AERODYNAMIC ANALYSIS OF WING-BODY-TAIL CONFIGURATIONS IN SUBSONIC AND SUPERSONIC FLOW

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BookPublisher: Nasa, Washington, D.C. 1973Description: 128.DDC classification: NASA | CR-2228

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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 CR-2228 (Browse shelf)	Not for loan		TR12999

Total holds: 0

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Previous	NASA CR-2225 ANALYSIS OF HELICOPTER MANEUVER-LOADS AND ROTOR-LOADS FLIGHT-TEST DATA	NASA CR-2226 DEVELOPMENT OF A HIGH SPEED PARALLEL HYBRID BOOST BEARING	NASA CR-2228 AN IMPROVED METHOD FOR THE AERODYNAMIC ANALYSIS OF WING-BODY-TAIL CONFIGURATIONS IN SUBSONIC AND SUPERSONIC FLOW	NASA CR-2228 AN IMPROVED METHOD FOR THE AERODYNAMIC ANALYSIS OF WING-BODY-TAIL CONFIGURATIONS IN SUBSONIC AND SUPERSONIC FLOW	NASA CR-2229 60 GHZ RADIOMETRIC LOCAL VERTICAL SENSOR EXPERIMENT	NASA CR-223 AN EXAMINATION OF THE APPLICABILITY OF MICROELECTRONIC CIRCUITS TO THE TELEMETRY AND COMMAND SUBSYSTEMS OF SEVERAL APPLICATIONS SPACECRAFT.	NASA CR-224 STRENGHT CHARACTERISTICS OF COMPOSITE MATERIALS.	Next

Bound With Nasa Cr-2221-27,2229

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