01771nam a2200397Ia 4500011447743MiAaHDL20141009010000.0m d cr bn ---auaua061207s1959 dcua bt f000 0 eng d89N7044219890068069sdr-uiuc6393221(OCoLC)76901598FERFERUIUUNewsom, William A.Wind-tunnel investigation of the aerodynamic characteristics of a model representative of a supersonic fighter-class airplane with an external-flow jet-augmented flap in low-speed flight /by William A. Newsom, Jr.Washington, [D.C.] :National Aeronautics and Space Administration,1959.84 p. :ill. ;26 cm.NASA technical note ;D-50"NASA TN D-50.""Langley Research Center, Langley Field, Va.""September 1959."Title from cover.Includes bibliographical references (p. 14).Also available online from the NASA Technical Reports Server (http://ntrs.nasa.gov/). Address as of 11/17/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19890068069_1989068069.pdf.Mode of access: Internet.Augmentation flaps (control surfaces)nasatAerodynamic forces.nasatAerodynamic characteristics.nasatWind tunnel tests.nasatWind tunnel models.nasatLow speed.nasatFighter aircraft.nasatExternally blown flaps.nasatLangley Research Center.01144774320101103124943.020141009010000.020141112165512.02025-01-02T19:06:04Z2025-01-02T18:30:02ZSDR-UIUCUNKNOWNloader.pl-003-020BKsdr-uiuc6393221uiugSDRUIUCuiug.30112106741108UIU6393221UIUUIUC20250102googleuiug.301121067411081959pdbibUS fed doc