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EFFECTS OF SUCTION ON THE INTERACTION BETWEEN SHOCK WAVE AND BOUNDARY LAYER AT A COMPRESSION CORNER.

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BookPublisher: Her Majesty'S Stationery Office, London 1970Description: 11.DDC classification: ARC | C.P. 1087

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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 C.P. 1087 (Browse shelf)	Not for loan		TR12183

Total holds: 0

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Previous	ARC C.P. 1084 COMPARISON OF DIFFERENT METHODS OF ASSESSING THE FREE OSCILLATORY CHARACTERISTICS OF AEROELASTIC SYSTEMS.	ARC C.P. 1085 ESTIMATION OF SURFACE PRESSURES FROM OBSERVED SHOCK-WAVE ENVELOPES SURROUNDING CONICAL BODIES AT M=4.0	ARC C.P. 1086 A THEORETICAL INVESTIGATION FOR DELTA WINGS WITH LEADING-EDGE SEPARATION AT LOW SPEEDS.	ARC C.P. 1087 EFFECTS OF SUCTION ON THE INTERACTION BETWEEN SHOCK WAVE AND BOUNDARY LAYER AT A COMPRESSION CORNER.	ARC C.P. 1088 CIVIL AIRCRAFT AIRWORTHINESS DATA RECORDING PROGRAMME SPECIAL EVENTS RELATED TO AIRSPEED CONTROL PRACTICES (FEBRUARY 1963 TO FEBRUARY 1966).	ARC C.P. 1090 A BRIEF ACCOUNT OF SOME UNRECORDED TECHNIQUES FOR FLOW VISUALIZATION IN FLIGHT FOR LOCATING (A) BOUNDARY-LAYER TRANSITION AT ALTITUDE, (B) SHOCK-WAVE POSITION.	ARC C.P. 1092 AN INFLATED MOBILE LIFTING SYSTEM FOR AN 8 TON LOAD.	Next

Bound With Arc C.P. 1081-86, 1088-90

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