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THE DEVELOPMENT OF A STATIC TUBE WHICH IS INSENSITIVE TO INCIDENCE AT SUPERSONIC SPEEDS.

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BookPublisher: Her Majesty'S Stationery Office, London 1960Description: 5.DDC classification: ARC | C.P. 543

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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. 543 (Browse shelf)	Not for loan Untraceable		TR10922

Total holds: 0

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Previous	ARC C.P. 539 THE ACCELERATION OF WATER DROPS BY AN AIRSTREAM OF CONSTANT RELATIVE VELOCITY.	ARC C.P. 540 A METHOD FOR DESIGNING BODY SHAPE TO PRODUCE PRESCRIBED PRESSURE DISTRIBUTIONS ON WING-BODY COMBINATIONS AT SUPERSONIC SPEEDS.	ARC C.P. 542 PRESSURE MEASUREMENTS AT THE CENTRE OF A 40 DEGREE SWEPT BACK WING WITH R.A.E. 101-10 SECTIONS AT ZERO INCIDENCE AND TRANSONIC SPEEDS.	ARC C.P. 543 THE DEVELOPMENT OF A STATIC TUBE WHICH IS INSENSITIVE TO INCIDENCE AT SUPERSONIC SPEEDS.	ARC C.P. 544 PRESSURE MEASUREMENTS ON THREE OPEN NOSE AIR INTAKES AT TRANSONIC AND SUPERSONIC SPEEDS, WITH AN ANALYSIS OF THEIR DRAG CHARACTERISTICS.	ARC C.P. 545 BEATING THE HEAT BARRIER.	ARC C.P. 546 EXPERIMENTAL STUDY OF THE FLOW OVER A PARTICULAR AFTERBODY SHAPE HAVING A NEAR-SONIC RIDGE LINE.	Next

Bound With Arc C.P.541-42, 544-50

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