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Browsing by Author "L.C. Squire"

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An experimental investigation of the characteristics of an ogee wing from M = 0.4 to M = 1.8

L.C. Squire; D.S. Capps (1962)
The influence of a model on plenum chamber indication of mach number in a slotted wall wind tunnel

L.C. Squire; A. Stanbrook (1958)
Wind tunnel tests at mach numbers up to 1.8 on a model with .03 scale wings and nacelles of a twin-engined supersonic aircraft (Bristol 188)

E.P. Sutton; P.G. Hutton; L.C. Squire (1965)

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