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COMPUTATION OF THE VELOCITY FIELD INDUCED BY A PLANAR SOURCE DISTRIBUTION APPROXIMATING A SYMMETRICAL NONLIFTING WING IN SUBSONIC FLOW

By: Ledger, J.A.

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BookSeries: Aeronautical Research Council Reports And Memoranda No. Rsm3751. Publisher: DDC classification: RSM3751

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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	RSM3751 (Browse shelf)	Not for loan Untraceable		TR6184

Total holds: 0

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Previous	RP-98 ALE SOLUTION OF AXISYMMETRIC PROBLEMS OF THE THEORY OF ELASTICITY WITH THE AID OF RELATIONS BETWEEN AXISYMMETRIC AND PLANE STATES OF STRESS	RP-99 MOS ENERGY TRANSFER BETWEEN A FLUID AND A ROTOR FOR PUMP AND TURBINE MACHINERY	RPPH54 - Limits on deritive couplings in the weak leptonic current	RSM3751 COMPUTATION OF THE VELOCITY FIELD INDUCED BY A PLANAR SOURCE DISTRIBUTION APPROXIMATING A SYMMETRICAL NONLIFTING WING IN SUBSONIC FLOW	RSM3752 NOTES ON THE APPROXIMATE SOLUTION OF LIFTING-SURFACE THEORY USED IN THE R.A.E. STANDARD METHOD	SAO SR-257 SATELLITE ORBITAL DATA.	SAO SR-258 AN ANALYSIS OF MARTIAN PHOTOMETRYAND POLARIMETRY.	Next

Bound With: Arc 3749-3759

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