Free-flight investigation at Mach numbers between 0.5 and 1.7 of the zero-lift rolling effectiveness and drag of various surface, spoiler, and jet controls on an 80° delta-wing missile / by Eugene D. Schult.
|Main Author:||Schult, Eugene D.|
Washington, [D.C.] : National Aeronautics and Space Administration, 1960.
Title from cover.
"Langley Research Center, Langley Field, Va."
Also available online from the NASA Technical Reports Server (http://ntrs.nasa.gov/). Address as of 1/04/07: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19890068625_1989068625.pdf.
"NASA TN D-205."
47 p. :
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