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AIRFOIL PROFILES FOR MINIMUM PRESSURE DRAG AT SUPERSONIC VELOCITIES - GENERAL ANALYSIS WITH APPLICATION TO LINEARIZED SUPERSONIC FLOW

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BookPublisher: Naca, Washington Description: 38.DDC classification: NACA | TN 2264

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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 2264 (Browse shelf)	Not for loan		TR15642

Total holds: 0

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Previous	NACA TN 2261 WIND-TUNNEL INVESTIGATION OF A NUMBER OF TOTAL-PRESSURE TUBES AT HIGH ANGLES OF ATTACK	NACA TN 2262 ROLLING AND YAWING MOMENTS FOR SWEPT-BACK WINGS IN SIDESLIP AT SUPERSONIC SPEEDS	NACA TN 2263 THE USE OF A LUMINESCENT LACQUER FOR THE VISUAL INDICATION OF BOUNDARY-LAYER TRANSITION	NACA TN 2264 AIRFOIL PROFILES FOR MINIMUM PRESSURE DRAG AT SUPERSONIC VELOCITIES - GENERAL ANALYSIS WITH APPLICATION TO LINEARIZED SUPERSONIC FLOW	NACA TN 2265 NACA VGH RECORDER	NACA TN 2267 INELASTIC COLUMN BEHAVIOR	NACA TN 2268 TESTS OF TWO-BLADE PROPELLERS IN THE LANGLEY 8-FOOT HIGH-SPEED TUNNEL TO DETERMINE THE EFFECT ON PROPELLER PERFORMANCE OF A MODIFICATION OF INBOARD PITCH DISTRIBUTION	Next

Bound With Naca Tn 2260-63,2265-70

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