01462cam a2200361Ma 4500011449547MiAaHDL20141009010000.0m d cr bn ---auaua011026s1971 dcua bt f000 0 eng dsdr-uiuc6403018(OCoLC)648098664TRLSTFUIUUTL500.T33 71-03798NAS 1.14:D-6393NASA-TN-D-6393Page, V. Robert.Stability and control characteristics of a large-scale deflected slipsteam STOL model with a wing of 5.7 aspect ratio /by V. Robert Page and Thomas N. Aiken.Washington, D.C. :National Aeronautics and Space Administration,1971.v, 62 p. :ill. ;27 cm.NASA technical note ;NASA TN D-6393Prepared at Ames Research Center.N71-36435.Includes bibliographical references (p. 6).Wind tunnel tests of stability and control characteristics of large scale model representative of propeller-driven STOL transport aircraft.Mode of access: Internet.Lift (Aeronautics)AirplanesWings.Short take-off and landing aircraft.Stability of airplanes.Aiken, Thomas N.United States.National Aeronautics and Space Administration.Ames Research Center.01144954720101110094236.020141009010000.020141112165512.02025-01-02T19:06:42Z2025-01-02T18:30:02ZSDR-UIUCUNKNOWNloader.pl-003-020BKsdr-uiuc6403018uiugSDRUIUCuiug.30112106747196UIU6403018UIUUIUC20250102googleuiug.301121067471961971pdbibUS fed doc