02124cam a2200493Ia 4500011429025MiAaHDL20141009010000.0m d cr bn ---auaua060508s1969 dcua bt f000 0 eng d19690029434N693881969N38819sdr-uiuc6380365(OCoLC)68478729FERFERLHLUIUUNAS 1.26:1426N69-3881969N38819NASA CR 1426Taylor, Charles R.Flight test results of a trailing edge flap designed for direct-lift control /by Charles R. Taylor.Washington, D.C. :National Aeronautics and Space Administration ;Springfield, Va. :For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor],1969.vi, 80 p. :ill. ;27 cm.NASA contractor report ;NASA CR-1426"NASA CR-1426.""October 1969"--Cover.Includes bibliographical references (p. 80).This report investigates boundary layer control and trailing edge flaps for direct-lift control.Also available online from the NASA Technical Reports Server (http://ntrs.nasa.gov/). Address as of 11/18/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19690029434%5F1969029434.pdf.Prepared by the Boeing Company, Seattle, Wash. for Ames Research CenterNAS 2-4200Mode of access: Internet.Flaps (Airplanes)Trailing edge flaps.AirplanesFlight testing.Turbulent boundary layer.Jet impingement.nasatDeceleration.nasatAerodynamic characteristics.nasatTrailing-edge flaps.nasatFlight tests.nasatBoundary layers.nasatBoeing Company.Ames Research Center.01142902520101022094405.020141009010000.020141112164151.02025-01-01T19:22:19Z2025-01-01T18:30:02ZSDR-UIUCUNKNOWNloader.pl-003-020BKsdr-uiuc6380365uiugSDRUIUCuiug.30112106624858UIU6380365UIUUIUC20250101googleuiug.301121066248581969pdbibUS fed doc