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TRANSONIC AERODYNAMIC CHARACTERISTICS OF A MODEL OF A PROPOSED SIX-ENGINE HULL-TYPE SEAPLANE DESIGNED FOR SUPERSONIC FLIGHT

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BookPublisher: Nasa, Washington, D.C. 1960Description: 38.DDC classification: NASA | TM X-246 -

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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-246 - (Browse shelf)	Not for loan		TR8829

Total holds: 0

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Previous	NASA TM X-235 - EXPERIMENTAL INVESTIGATION AND CORRELATION OF THE HEAT REDUCTION TO NONPOROUS SURFACES BEHIND A POROUS LEADING EDGE THROUGH WHICH COOLANT IS EJECTED	NASA TM X-24 - AERODYNAMIC CHARACTERISTICS OF A 0.0667-SCALE MODEL OF THE NORTH AMERICAN X-15 RESEARCH AIRPLANE AT TRANSONIC SPEEDS	NASA TM X-240 - HYPERSONIC LONGITUDINAL TRIM, STABILITY, AND CONTROL CHARACTERISTICS OF A DELTA-WING CONFIGURATION AT HIGH ANGLES OF ATTACK	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	Next

Bound With Nasa Tm X-205-49

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