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: prepared for Langley Research Center.
Contributors: Fiscko, K. A.; Langley Research Center
Publisher: Langley Research Center
Published: 1979
Place of publication: Hampton, Va
Number of pages: 112
Subjects: Force distribution; Pressure distribution; Wind tunnel tests
Notes: Includes bibliographical references.