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1. DYNAMIC STABILITY DERIVATIVES OF A SLENDER WING, A COMPARISON OF THEORY WITH FREE-FLIGHT MODEL TESTS AT NEAR-ZERO LIFT M = 0.8 TO 2.4

by Turner,K. J., Ross,A. Jean | Earley,Geraldine.

Material type: book Book Description: 67.Publisher: Her Majesty'S Stationery Office, London 1968Availability: No items available Damaged (1).

2. MEASUREMENTS OF PRESSURE FLUCTUATION AND SKIN FRICTION ON THE UPPER SURFACE OF A SLENDER WING AT LIFT (M=0.8 TO 2.0)

by Turner,K J | Walker,D.

Material type: book Book Description: 25.Publisher: Her Majesty'S Stationery Office, London 1966Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: ARC C.P. 985] (1).

3. A ROLL-BALANCE FREE-FLIGHT TEST VEHICLE FOR THE MEASUREMENT OF AILERON ROLLING POWER AND ROLL DAMPING AT M-O.8 TO 2.5

by Turner,K J.

Material type: book Book Description: 10.Publisher: Her Majesty'S Stationery Office, London 1958Availability: No items available Damaged (1).

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