01908nam a2200469Ia 4500011445822MiAaHDL20141009010000.0m d cr bn ---auaua070108s1960 dcua bt f000 0 eng d89N7099819890068625sdr-uiuc6394768(OCoLC)77551527FERFERUIUUSchult, Eugene D.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.Washington, [D.C.] :National Aeronautics and Space Administration,1960.47 p. :ill. ;26 cm.NASA technical note ;D-205"NASA TN D-205.""Langley Research Center, Langley Field, Va.""February 1960."Title from cover.Includes bibliographical references (p. 22-23).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.Mode of access: Internet.Wedge flow.nasatWakes.nasatTrailing edges.nasatThrust control.nasatSubsonic speed.nasatMach number.nasatZero lift.nasatSpoilers.nasatSpanwise blowing.nasatJet control.nasatFree flight.nasatDrag.nasatDelta wings.nasatControl surfaces.nasatLangley Research Center.01144582220101104121542.020141009010000.020141112165512.02025-01-01T19:19:15Z2025-01-01T18:30:02ZSDR-UIUCUNKNOWNloader.pl-003-020BKsdr-uiuc6394768uiugSDRUIUCuiug.30112106588236UIU6394768UIUUIUC20250101googleuiug.301121065882361960pdbibUS fed doc