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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]

By: Jackson, Charlie M.

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BookSeries: National Aeronautics and Space Administration ; NASA Technical Note. Publisher: Washington, D.C. National Aeronautics and Space Administration 1961Description: 18p.Subject(s): Arbitrary body

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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 791-800	Not for loan		TR8254

Total holds: 0

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Previous	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]	Residual static strength of aluminium alloy box beams containing fatigue cracks in the tension covers [NASA TN D-796]	The magnetic field on the axis of circular cylindrical coils[NASA TN D-1013]	Experimental separation for two-dimensional wedges and curved surfaces at mach numbers of 4.8 to 6.2[NASA TN D-1014]	Next

Bound With NASA TN D 791-800

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