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NUMERICAL SOLUTION OF THE FLOW OF A PERFACT GAS OVER A CIRCULAR CYLINDER AT INFINITE MACH NUMBER

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BookPublisher: Nasa, Washington, D.C. 1959Description: 33.DDC classification: NASA | MEMO 2-25-59A -

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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 MEMO 2-25-59A - (Browse shelf)	Not for loan		TR7525

Total holds: 0

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Previous	NASA MEMO 2-24-59A - EFFECT OF MOMENT-OF AREA-RULE MODIFICATIONS ON THE DRAG, LIFT, AND PITCHING-MOMENT CHARACTERISTICS OF AN UNSWEPT ASPECT-RATIO-6 WING AND BODY COMBINATION	NASA MEMO 2-24-59L - BASIC PRESSURE MEASUREMENTS AT TRANSONIC SPEEDS ON A THIN 45(DEGREE) SWEPTBACK HIGHLY TAPERED WING WITH SYSTEMATIC SPANWISE TWIST VARIATIONS	NASA MEMO 2-24-59W - THEORETICAL DETERMINATION OF LIFETIME OF COMPRESSED PLATES AT ELEVATED TEMPERATURES	NASA MEMO 2-25-59A - NUMERICAL SOLUTION OF THE FLOW OF A PERFACT GAS OVER A CIRCULAR CYLINDER AT INFINITE MACH NUMBER	NASA MEMO 2-25-59E HALOGEN-CONTAINING GASES AS BOUNDARY LUBRICANTS FOR CORROSION-RESISTANT ALLOYS AT 1200 DEGREE F	NASA MEMO 2-25-59L - SEVERAL METHODS FOR REDUCING THE DRAG OF TRANSPORT CONFIGURATIONS AT HIGH SUBSONIC SPEEDS	NASA MEMO 2-26-59A - SOME FINITE DIFFERENCE SOLUTIONS OF THE LAMINAR COMPRESSIBLE BOUNDARY LAYER SHOWING THE EFFECTS OF UPSTREAM TRANSPIRATION COOLING	Next

Bound With Nasa Memo 2-3-59a-2-27-59a

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