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A technique for the measurement of pressure distribution on oscillating aerofoils, with results for a rectangular wing of aspect ratio 3.3
W. G. Molyneux
;
F. Ruddlesden
(
1955
)
Derivative measurements and flutter tests on a rectangular wing with a full-span control surface, oscillating in modes of wing roll and aileron rotation
W. G. Molyneux
;
F. Ruddlesden
(
1955
)
Flutter tests on some delta wings using ground-launched rockets
W. G. Molyneux
;
F. Ruddlesden
(
1955
)
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Author
F. Ruddlesden (3)
W. G. Molyneux (3)
Date Issued
1955 (3)