Force and pressure-distribution measurements on a rectangular wing with a slotted droop nose and with either plain and split flaps in combination or a slotted flap /

Force measurements and pressure distribution measurements on the midsection were made on a rectangular wing with slotted droop nose and end plates, on which could be placed a choice of either a plain flap-split flap combination or a slotted flap

Bibliographic Details
Main Author: Lemme, H. G
Corporate Author: United States National Advisory Committee for Aeronautics
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, [1947]
Series:Technical memorandum (United States. National Advisory Committee for Aeronautics) ; no. 1108
Subjects:

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Stanford University

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Call Number: ISIL:US-CST
NACA TM 1108