Analysis of factors affecting net lift increment attainable with trailing-edge split flaps on tailless airplanes
Publisher: NACA
Published: 1944
Place of publication: Washington, D.C.
Language: eng
Number of pages: 58
Subjects: Aeronautics--Research; Airplanes, Tailless; Lift (Aerodynamics; Trailing edge flaps--Aerodynamics.
Description: <a href="http://uf.catalog.fcla.edu/uf.jsp?st=UF003804825&ix=nu&I=0&V=D&pm=1" rel="nofollow">http://uf.catalog.fcla.edu/uf.jsp?st=UF003804825&ix=nu&I=0&V=D&pm=1</a>