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SUPERSONIC WIND TUNNEL TESTS ON A 1/12TH SCALE MODEL OF THE BRISTOL TYPE 188 RESEARCH AIRCRAFT PART 2 : M=2.0 TO 2.7.

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BookPublisher: Her Majesty'S Stationery Office, London 1965Description: 17.DDC classification: ARC | C.P. 818S

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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. 818S (Browse shelf)	Not for loan		TR11065

Total holds: 0

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Previous	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.	ARC C.P. 820 ANALYSIS OF FLIGHT LOADS RECORDED ON COMET 4B AIRCRAFT BY MEANS OF THE FATIGUE LOAD METER.	ARC C.P. 822 THE STATIC PRESSURE DISTRIBUTION AROUND A CIRCULAR JET EXHAUSTING NORMALLY FROM A PLANE WALL INTO AN AIRSTREAM.	Next

Bound With Arc C.P. 800-818, 819-20 Lack No. 801-4,9,15-16.

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