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Aerodynamics influence coefficient method using singularity splines [NASA CR-2423]

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BookSeries: National Aeronautics and Space Administration (NASA). Publisher: Washington, D. C. NASA May 1974Description: 100p.Subject(s): Aerodynamic influence

Contents:

NASA contractor report

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)		Not for loan		TR007936 [CR-2423]

Total holds: 0

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Previous	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]	TRANSONIC WIND-TUNNEL INVESTIGATION OF THE STATIC LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF SEVERAL CONFIGURATIONS OF THE SCOUT VEHICLE AND OF A NUMBER OF RELATED MODELS [NASA TN D-794]	A SEMIGRAPHICAL METHOD OF APPLYING IMPACT THEORY TO AN ARBITRARY BODY TO OBTAIN THE HYPERSONIC AERODYNAMIC CHARACTERISTICS AT ANGLE OF ATTACK AND SIDESLIP [NASA TN D-795]	Next

NASA contractor report

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