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WIND TUNNEL TESTS ON A 1/12TH SCALE MODEL OF THE BRISTOL TYPE 188 RESEARCH AIRCRAFT WITH RECTANGULAR, WEDGE INTAKES AT MACH NUMBERS FROM 2.0 TO 2.7.

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BookPublisher: Her Majesty'S Stationery Office, London 1965Description: 12.DDC classification: ARC | C.P. 817

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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. 817 (Browse shelf)	Not for loan Untraceable		TR11063

Total holds: 0

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Previous	ARC C.P. 812 INFLUENCE OF CHEMICAL CONTOURING ON THE FATIGUE AND SUSTAINED LOAD PROPERTIES OF HIGH TENSILE STEEL SHEET.	ARC C.P. 813 THEORETICAL INVESTIGATION OF SOME BASIC ASSUMPTION OF SCHLICHTING'S SINGULARITY METHOD OF CASCADE ANALYSIS.	ARC C.P. 814 MEASUREMENTS OF SKIN-FRICTION IN AN ANNULUS BY THE FLOATING ELEMENT TECHNIQUE.	ARC C.P. 817 WIND TUNNEL TESTS ON A 1/12TH SCALE MODEL OF THE BRISTOL TYPE 188 RESEARCH AIRCRAFT WITH RECTANGULAR, WEDGE INTAKES AT MACH NUMBERS FROM 2.0 TO 2.7.	ARC C.P. 818 SUPERSONIC WIND TUNNEL TESTS ON A 1/12TH SCALE MODEL OF THE BRISTOL TYPE 188 RESEARCH AIRCRAFT PART 1	ARC C.P. 818S SUPERSONIC WIND TUNNEL TESTS ON A 1/12TH SCALE MODEL OF THE BRISTOL TYPE 188 RESEARCH AIRCRAFT PART 2	ARC C.P. 819 ALLEVIATION OF THERMAL STRESSES IN AIRCRAFT STRUCTURES.	Next

Bound With Arc C.P. 800-814, 818-20 Lack No. 801-4,9,15-16.

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