Wind tunnel force and pressure tests of a 21% thick general aviation airfoil with 20% aileron, 25% slotted flap and 10% slot-lip spoiler
An edition of Wind tunnel force and pressure tests of a 21% thick general aviation airfoil with 20% aileron, 25% slotted flap and 10% slot-lip spoiler (1979)
By W. H. Wentz
Publish Date
1979
Publisher
Langley Research Center
Language
-
Pages
112
1-1 of 1 Editions
Wind tunnel force and pressure tests of a 21% thick general aviation airfoil with 20% aileron, 25% slotted flap and 10% slot-lip spoiler
Pages: 112
Published In: 1979
Publisher: Langley Research Center