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LOW-SPEED WIND-TUNNEL MEASUREMENTS OF THE OSCILLATORY LATERAL STABILITY DERIVATIVES FOR A MODEL OF A SLENDER AIRCRAFT ( HP 115) INCLUDING THE EFFECTS OF FREQUENCY PARAMETER

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BookPublisher: Her Majesty'S Stationery Office, London 1970Description: 30.DDC classification: ARC | C.P 1097

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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 1097 (Browse shelf)	Not for loan		TR9263

Total holds: 0

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Previous	ARC-C.P 1040 THE DRAG OF INFINTE SWEPT WINGS WITH AN ADDENDUM	ARC C.P 1094 CABIN AIR REQUIREMENTS FOR CREW COMFORT IN MILITARY AIRCRAFT.	ARC C.P 1096 LAMINAR BOUNDARY-LAYER CALCULATIONS COMPARED WITH MEASUREMENTS BY HUMMEL.	ARC C.P 1097 LOW-SPEED WIND-TUNNEL MEASUREMENTS OF THE OSCILLATORY LATERAL STABILITY DERIVATIVES FOR A MODEL OF A SLENDER AIRCRAFT ( HP 115) INCLUDING THE EFFECTS OF FREQUENCY PARAMETER	ARC C.P 1182 CIVIL AIRCRAFT AIRWORTHINESS DATA RECORDING PROGRAMME HARD LANDING ENCOUNTARED BY SUBSONIC CIVIL JET AIRFCRAFT.	ARC C.P 1183 VERTICAL COCKPIT ACCELERATIONS MEASURED ON AN OPERATIONAL JET TRANSPORT AIRCRAFT.	ARC C.P 1184 AN INVESTIGATION OF THE PRESSURE DISTRIBUTIONS ON A 45 DEGREE SWEPT HALF WING INCLUDING THE EFFECTS OF UPPER SURFACE SPOLIERS.	Next

Bounds With Arc C.P.1091-96,1098-99

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