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THE DEVELOPMENT AT CRANFIELD OF A FREE PISTON COMPRESSION SHOCK TUBE.

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BookPublisher: Her Majesty'S Stationery Office, London 1967Description: 14.DDC classification: ARC | C.P. 1002

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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. 1002 (Browse shelf)	Not for loan Untraceable		TR10827

Total holds: 0

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Previous	ARC C. P. 1012 FURTHER MEASUREMENTS OF TRANSIENT PRESSURES ON A NARROW-DELTA WING DUE TO A VERTICAL GUST	ARC C. P. 622 QUALITATIVE SOLUTION OF THE STABILITY EQATION FOR A BOUNDARY LAYER IN CONTACT WITH VARIOUS FORMS OF FLEXIBLE SURFACE.	ARC C.P. 1001 THE PILOT`S SAFETY PROBLEM IN CATEGORY II OPERATIONS AND THE POTENTIAL CONTRIBUTION OF HEAD-UP DISPLAY.	ARC C.P. 1002 THE DEVELOPMENT AT CRANFIELD OF A FREE PISTON COMPRESSION SHOCK TUBE.	ARC C.P. 1003 AIRCRAFT LOADING ACTIONS PROBLEMS - PROCEEDINGS OF A SYMPOSIUM HELD AT FARNBOROUGH ON 28TH OCT.1966.	ARC C.P. 1004 THE NEW SYSTEM FOR CONTROLLING THE ATTITUDE AND MOTIVATOR DEFLECTIONS OF A MODEL IN THE R.A.E. NO.19 WIND TUNNEL.	ARC C.P. 1005 THE CALCULATION OF THE PRESSURE DISTRIBUTION ON A THICK CAMBERED AEROFOIL AT SUBSONIC SPEEDS INCLUDING THE EFFECTS OF THE BOUNDARY LAYER.	Next

Bound With Arc C.P.1000-1001, 1003-1009

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