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EFFECT OF MULTIPLE-JET EXITS ON THE BASE PRESSURE OF A SIMPLE WING-BODY COMBINATION AT MACH NUMBERS OF 0.6 TO 1.27

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BookPublisher: Nasa, Washington, D.C. 1959Description: 36.DDC classification: NASA | TM X-25 -

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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-25 - (Browse shelf)	Not for loan Untraceable		TR9326

Total holds: 0

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Previous	NASA TM X-246 - TRANSONIC AERODYNAMIC CHARACTERISTICS OF A MODEL OF A PROPOSED SIX-ENGINE HULL-TYPE SEAPLANE DESIGNED FOR SUPERSONIC FLIGHT	NASA TM X-248 - ANALYSIS OF THE STABILITY OF SPINNING DISKS DURING ATMOSPHERIC REENTRY	NASA TM X-249 - AERODYNAMIC AND HYDRODYNAMIC CHARACTERISTICS OF A PROPOSED SUPERSONIC MULTIJET WATER-BASED HULL-TYPE AIRPLANE WITH A VARIABLE-INCIDENCE WING	NASA TM X-25 - EFFECT OF MULTIPLE-JET EXITS ON THE BASE PRESSURE OF A SIMPLE WING-BODY COMBINATION AT MACH NUMBERS OF 0.6 TO 1.27	NASA TM X-26 - DESIGN GUIDE FOR PITCH-UP EVALUATIO AND INVESTIGATION AT HIGH SUBSONIC SPEEDS OF POSSIBLE LIMITATIONS DUE TO WING-ASPECT-RATIO VARIATIONS	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	Next

Bound With Nasa Tm X-22-39

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