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Measurements of Velocity Fluctuations in the Working Section of the R.A.E. 4ft.x 3ft. Wind Tunnel with Flow Disturbances in the Second Diffuser
J. A. Lawford
(
1959
)
Low-speed wind-tunnel tests on an unswept wing-fuselage model of aspect ratio 9.8, with tangential blowing over trailing-edge flaps and ailerons, including the effect of slipstream
J. A. Lawford
(
1970
)
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J. A. Lawford (2)
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1960 - 1970 (1)
1959 - 1959 (1)