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AERODYNAMIC-DERIVATIVE CHARACTERISTICS OF THE X-15 RESEARCH AIRPLANE AS DETERMINED FROM FLIGHT TESTS FOR MACH NUMBERS FROM 0.6 TO 3.4 [NASA TN D-1010]

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BookPublisher: Washington, D.C. National Aeronautics and Space Administration 1962Description: 68p.Subject(s): Aerodynamic

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Item type	Current location	Collection	Call number	Vol info	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)		NASA TN D-1051-1060	Not for loan		TR7923

Total holds: 0

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Previous	NASA Technical Note [NASA TN D-3125]: A new approach to the explanation of the flutter mechanism	CORROSION STUDY OF BARE AND COATED STAINLESS STEEL	Trace organic impurities in gaseous helium [ NASA TN D-6520]	AERODYNAMIC-DERIVATIVE CHARACTERISTICS OF THE X-15 RESEARCH AIRPLANE AS DETERMINED FROM FLIGHT TESTS FOR MACH NUMBERS FROM 0.6 TO 3.4 [NASA TN D-1010]	The effect of yttrium and thorium on the oxidation behavior of Ni-Cr-Al alloys [NASA CR-2422]	Aerodynamics influence coefficient method using singularity splines [NASA CR-2423]	An economic assessment of stol aircraft potential including thermal area environmental considerations [NASA CR-2424]	Next

Bound With NASA TN D-1051-1060

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