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LIFTING SURFACE THEORY METHOD FOR TREATING SWEPT OR SLENDER WINGS IN ATTACHED SUBSONIC FLOW

By: Kellaway,W.

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BookSeries: Aeronautical Research Council Reports And Memoranda R&M3760. Publisher: DDC classification: R&M3760

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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	R&M3760 (Browse shelf)	Not for loan		TR6193

Total holds: 0

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Previous	R&M3757 FORM OF THE SUPERSONIC FLOW EQUATIONS FOR AN IDEAL GAS	R&M3758 ON THE APPLICATION OF SUBSONIC LINEARISED WING THEORY TO SECOND ORDER FORCES AND MOMENTS	R&M3759 SECOND ORDER SMALL PERTURBATION THEORY FOR FINITE WINGS IN INCOMPRESSIBLE FLOW	R&M3760 LIFTING SURFACE THEORY METHOD FOR TREATING SWEPT OR SLENDER WINGS IN ATTACHED SUBSONIC FLOW	R&M3761 AUTHOR INDEX TO THE REPORT AND MEMORANDA AND CURRENT PAPERS OF THE AERONAUTICAL RESEARCH COUNCIL	R&M-3762 NEW PROBE FOR THE DIRECT MEASUREMENT OF STAGNATION PRESSURE IN SUPERSONIC FLOW	R&M-3763 MEASUREMENTS IN LOW SPEED FLOW OF UNSTEADY PRESSURE DISTRIBUTIONS ON A RECTANGULAR WING WITH AN OSCILLATING CONTROL SURFACE	Next

Bound With :Arc R&M3760-3769

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