The Online Books Page

Online Books by

Irving Abel

Books from the extended shelves:

• Abel, Irving: An analytical technique for predicting the characteristics of a flexible wing equipped with an active flutter-suppression system and comparison with wind-tunnel data / ([Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Office, 1979) (page images at HathiTrust)
• Abel, Irving: Application of two design methods for active flutter suppression and wind-tunnel test results / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1980), also by Jerry R. Newsom, H. J. Dunn, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Abel, Irving: Comparison of analytical and wind-tunnel results for flutter and gust response of a transport wing with active controls / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982), also by Jerry R. Newsom, Boyd Perry, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Abel, Irving: Development and application of an optimization procedure for flutter supression using the aerodynamic energy concept / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), also by E. Nissim and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Abel, Irving: Development and demonstration of a flutter-suppression system using active controls / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), also by M. C. Sandford, David L. Gray, and Langley Research Center (page images at HathiTrust)
• Abel, Irving: Evaluation of a technique for determining airplane aileron effectiveness and roll rate by using an aeroelastically scaled model / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), also by Langley Research Center and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Abel, Irving: Flutter studies of simplified component models of a variable-sweep-wing airplane at Mach numbers up to 3.0 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1966), also by M. C. Sandford, Charles L. Ruhlin, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Abel, Irving: A Method for obtaining reduced-order control laws for high-order systems using optimization techniques / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981), also by Vivek Mukhopadhyay, Jerry R. Newsom, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Abel, Irving: Transonic flutter study of a 50.5 ̊cropped-delta wing with two rearward-mounted nacelles / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), also by M. C. Sandford, Charles L. Ruhlin, and Langley Research Center (page images at HathiTrust)
• Abel, Irving: A wind-tunnel evaluation of analytical techniques for predicting static stability and control characteristics of flexible aircraft / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1972), also by Langley Research Center and United States National Aeronautics and Space Administration (page images at HathiTrust)

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