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Experimental separation for two-dimensional wedges and curved surfaces at mach numbers of 4.8 to 6.2[NASA TN D-1014]

By: Sterrett,James R.

Contributor(s): Emery,James C.

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BookSeries: National Aeronaitics and Space Adminstration ; NASA Technical Note. Publisher: Washington, D.C. National Aeronaitics and Space Adminstration 1962Description: 51p.Subject(s): Mental separation stuides

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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 1011-1020	Not for loan		TR10371

Total holds: 0

Browsing PK Kelkar Library, IIT Kanpur Shelves , Collection code: COMPACT STORAGE (BASEMENT) Close shelf browser

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Previous	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]	Theoretical evaluation of hypersonic forces, moments, and stability derivatives for a combination of flat plates, including effects of blunt leading edges by Newtonian impact theory[NASA TN D-1015]	Jet effects on cylindrical afterbodies housing sonic and supersonic nozzles which exhaust against a supersonic stream at angles of attack from 90 degree to 180 degree [NASA TN D-1016]	Exploratory investigation of jet-blast effects on a dust-covered surface at low ambient pressure[NASA TN D -1017]	Next

Bound vol. contains D 7831- 7835

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