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A METHOD FOR CALCULATING THE CONTOUR OF BODIES OF REVOLUTION WITH A PRESCRIBED PRESSURE GRADIENT AT SUPERSONIC SPEED WITH EXPERIMENTAL VERIFICATION

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BookPublisher: Naca, Washington 1955Description: 64.DDC classification: NACA | TN 3555

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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	NACA TN 3555 (Browse shelf)	Not for loan		TR14823

Total holds: 0

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Previous	NACA TN 3552 INVESTIGATION OF THE COMPRESSIVE STRENGTH AND CREEP LIFETIME OF 2024-T3 ALUMINUM-ALLOY PLATES AT ELEVATED TEMPERATURES 1	NACA TN 3553 COMPRESSIVE CRIPPLING OF STRUCTURAL SECTIONS	NACA TN 3554 A PRELIMINARY INVESTIGATION OF THE EFFECTS OF FREQUENCY AND AMPLITUDE ON THE ROLLING DERIVATIVES OF AN UNSWEPT-WING MODEL OSCILLATING IN ROLL	NACA TN 3555 A METHOD FOR CALCULATING THE CONTOUR OF BODIES OF REVOLUTION WITH A PRESCRIBED PRESSURE GRADIENT AT SUPERSONIC SPEED WITH EXPERIMENTAL VERIFICATION	NACA TN 3556 GRAIN-BOUNDARY BEHAVIOR IN CREEP OF ALUMINUM BICRYSTALS	NACA TN 3557 A THEORETICAL ANALYSIS OF THE FIELD OF A RANDOM NOISE SOURCE ABOVE AN INFINITE PLANE	NACA TN 3558 HEAT CAPACITY LAG OF GASEOUS MIXTURES	Next

Bound With Naca Tn 3550-3554,3556-3559

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