The Online Books Page

Online Books by

F. Edward Ehlers

Books from the extended shelves:

• Ehlers, F. Edward: Computation of the transonic perturbation flow fields around two- and three-dimensional oscillating wings (National Aeronautics and Space Administration ;, 1975), also by W. H. Weatherill, James D. Sebastian, Langley Research Center, and Boeing Commercial Airplane Company (page images at HathiTrust)
• Ehlers, F. Edward: Coupling linearized far-field boundary conditions with nonlinear near-field solutions in transonic flow (Bolling Air Force Base, D. C. : Air Force Office of Scientific Research, United States Air Force, 1988., 1988), also by William Rowe, Boeing Commercial Airplane Company, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• Ehlers, F. Edward: A finite difference method for the solution of the transonic flow around harmonically oscillating wings (National Aeronautics and Space Administration ;, 1974), also by Langley Research Center and Boeing Commercial Airplane Company (page images at HathiTrust)
• Ehlers, F. Edward: A harmonic analysis method for unsteady transonic flow and its application to the flutter of airfoils (National Aeronautical and Space Administration, Scientific and Technical Information Branch ;, 1982), also by W. H. Weatherill, Boeing Commercial Airplane Company, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Ehlers, F. Edward: A method for computing the leading-edge suction in a higher-order panel method (National Aeronautical and Space Administration, Scientific and Technical Information Office ;, 1984), also by Marjorie E. Manro, Boeing Commercial Airplane Company, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Langley Research Center (page images at HathiTrust)
• Ehlers, F. Edward: The practical application of a finite difference method for analyzing transonic flow over oscillating airfoils and wings (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by James D. Sebastian, Boeing Commercial Airplane Company, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)

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