01420cam a2200337Ia 4500011427754MiAaHDL20141013010000.0m d cr bn ---auaua810615s1980 dcua b f000 0 eng dsdr-uiuc6369890(OCoLC)7503108GPOGPOOCLABCOCLUIUUTL521.3.N18 no. 1777830-H-15 (microfiche)NAS 1.60:1777Coe, Paul L.Leading-edge deflection optimization for a highly swept arrow-wing configuration /Paul L. Coe, Jr., Jarrett K. Huffman, and James W. Fenbert.Washington, D.C. :National Aeronautics and Space Administration, Scientific and Technical Information Branch ;[Springfield, Va. :For sale by the National Technical Information Service],1980.56 p. :ill. ;27 cm.NASA technical paper ;1777Dec. 1980."Langely Research Center, Hampton, Virginia."Includes bibliographical references.Mode of access: Internet.Leading edges (Aerodynamics)AirplanesWings, Swept-back.Aerodynamics.Fenbert, James W.Huffman, Jarrett K.Langely Research Center.United States.National Aeronautics and Space Administration.Scientific and Technical Information Branch.01142775420101012141916.020141013010000.020141112173021.02025-01-01T19:18:05Z2025-01-01T18:30:02ZSDR-UIUCUNKNOWNloader.pl-003-020BKsdr-uiuc6369890uiugSDRUIUCuiug.30112106571349UIU6369890UIUUIUC20250101googleuiug.301121065713491980pdbibUS fed doc--NTIS: pubdate < 2020