Analysis of airplane "stalling point"; various tests on slotted and unslotted wings; calculation of lift coefficient of individual wings; combined usage of both slot and flap; lift properties of slotted wings of Handley Page H.P. 42 illustrating advantages of slots to airplane of large dimensions.
Problems of lift and stability in aeroplane design
Roy Philosphical Soc Glasgow -- Proc
1932
20 pages
Article (Journal)
English
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