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THE EFFECT OF A SPIKE PROTRUDING IN FRONT OF A BLUFF BODY AT SUPERSONIC SPEEDS.

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BookPublisher: Her Majesty'S Stationery Office, London 1957Description: 26.DDC classification: ARC | R&M 3007

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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	ARC R&M 3007 (Browse shelf)	Not for loan Untraceable		TR11042

Total holds: 0

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Previous	ARC R&M 3004 THE INTERACTION BETWEEN SHOCK WAVES AND BOUNDARY LAYERS AT THE TRAILING EDGE OF A DOUBLE-WEDGE AEROFOIL AT SUPERSONIC SPEED.	ARC R&M 3005 EFFECT OF YAW ON THE COMPRESSIBLE LAMINAR BOUNDARY LAYER.	ARC R&M 3006 THE THREE-DIMENSIONAL BOUNDARY-LAYER EQUATIONS AND SOME POWER SERIES SOLUTIONS.	ARC R&M 3007 THE EFFECT OF A SPIKE PROTRUDING IN FRONT OF A BLUFF BODY AT SUPERSONIC SPEEDS.	ARC R&M 3008 VELOCITY DISTRIBUTION ON THIN TAPERED ARROWHEAD AND DELTA WINGS WITH SPANWISE CONSTANT THICKNESS RATIO AT ZERO INCIDENCE.	ARC R&M 3009 LOW-SPEED WIND-TUNNEL MEASUREMENTS OF LONGITUDINAL OSCILLATORY DERIVATIVES ON THREE WING PLAN-FORMS.	ARC R&M 3010 DERIVATIVE MEASUREMENTS AND FLUTTER TESTS ON A RECTANGULAR WING WITH A FULLL-SPAN CONTROL SURFACE, OSCILLATING IN MODES OF WING ROLL AND AILERON ROTATION.	Next

Bound With Arc R&M 3000-3006, 3008-19 Lack No.3003,13,15.

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