The Online Books Page

Books by Arthur L. Jones:

Books in the extended shelves:

• Jones, Arthur L.: The effects of sideslip, aspect ratio, and Mach number on the lift and pitching moment of triangular, trapezoidal, and related plan forms in supersonic flow (National Advisory Committee for Aeronautics, 1949), also by Elizabeth E. Lindler, Robert M. Sorenson, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Jones, Arthur L.: Gust alleviation study : Part I. Estimation of the control derivatives for flaps, spoilers and other control devices intended for use as gust alleviators (Wright Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1958., 1958), also by Douglas C. Nichols, Charles D. Christopherson, Owen P. Lamb, A. E. Cronk, United States. Air Force. Air Research and Development Command, Wright Air Development Center, and Fluidyne Engineering Corporation (page images at HathiTrust)
• Jones, Arthur L.: Gust alleviation study : Part II. Prediction of the alleviation of gust loads on a rigid restrained wing utilizing wing installed alleviator devices (Wright Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1958., 1958), also by Douglas C. Nichols, Charles D. Christopherson, United States. Air Force. Air Research and Development Command, Wright Air Development Center, and Fluidyne Engineering Corporation (page images at HathiTrust)
• Jones, Arthur L.: A survey of stability analysis techniques for automatically controlled aircraft (National Advisory Committee for Aeronautics, 1951), also by Benjamin R. Briggs and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Jones, Arthur L.: Volterra's solution of the wave equation as applied to three-dimensional supersonic airfoil problems (National Advisory Committee for Aeronautics, 1947), also by Max A. Heaslet, Harvard Lomax, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Jones, Arthur L.: The yawing moment, due to sideslip of triangular, trapezoidal, and related plan forms in supersonic flow (National Advisory Committee for Aeronautics, 1949), also by Alberta Alksne and United States National Advisory Committee for Aeronautics (page images at HathiTrust)

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