Determination of the stability and control characteristics of a tailless all-wing airplane model with sweepback in the Langley free-flight tunnel
Publisher: Langley Memorial Aeronautical Laboratory
Published: 1945
Place of publication: Langley Field, VA
Language: eng
Number of pages: 42
Subjects: Airplanes, Tailless; Aerodynamics--Research.
Description: <a href="http://uf.catalog.fcla.edu/uf.jsp?st=UF003616137&ix=nu&I=0&V=D&pm=1" rel="nofollow">http://uf.catalog.fcla.edu/uf.jsp?st=UF003616137&ix=nu&I=0&V=D&pm=1</a>