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W. H. Wentz

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Additional flow field studies of the GA(W)-1 airfoil with 30-percent chord Fowler flap including slot-gap variations and cove shape modifications

by W. H. Wentz First published in 1983
2 editions

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Force and pressure tests on the GA(W)-1 airfoil with a 20 % aileron and pressure tests with a 30 % Fowler flap

by W. H. Wentz First published in 1977
1 edition

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Wind tunnel force and pressure tests of a 21% thick general aviation airfoil with 20% aileron, 25% slotted flap and 10% slot-lip spoiler

by W. H. Wentz First published in 1979
1 edition

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Pressure distributions for the GA(W)-2 airfoil with 20% aileron, 25% slotted flap and 30% Fowler flap

by W. H. Wentz First published in 1978
1 edition

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OLID: OL4821193A

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