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DESIGN GUIDE FOR PITCH-UP EVALUATIO AND INVESTIGATION AT HIGH SUBSONIC SPEEDS OF POSSIBLE LIMITATIONS DUE TO WING-ASPECT-RATIO VARIATIONS

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BookPublisher: Nasa, Washington, D.C. 1959Description: 37.DDC classification: NASA | TM X-26 -

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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-26 - (Browse shelf)	Not for loan Untraceable		TR9327

Total holds: 0

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Previous	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	NASA TM X-28 - DESIGN ANALYSIS OF A SUBSONIC NUCLEAR-POWERED LOGISTIC AIRPLANE WITH HELIUM-COOLED REACTOR	Next

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