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Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory
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Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory: Application of numerical integration techniques to the low-aspect-ratio flutter problem in subsonic and supersonic flows (Department of Aeronautical Engineering, Massachusetts Institute of Technology, 1954), also by Herbert M. Voss, Garabed Zartarian, and Pao Tan Hsu (page images at HathiTrust)- Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory: Development of a miniature pressure transducer for application to airfoil studies in the shock tube (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1958., 1958), also by J. Ray Ruetenik, United States. Air Force. Air Research and Development Command, and Wright Air Development Center (page images at HathiTrust)
- Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory: Dynamic response of shells to externally-applied dynamic loads (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), also by John W. Leech, Walter Herrmann, Emmett A. Witmer, Theodore H. H. Pian, Air Force Flight Dynamics Laboratory (U.S.), and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
- Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory: Effect of structural flexibiligy on aircraft loading. Part II, Spanwise airload distribution (Wright-Patterson Air Force Base, Ohio : United States, Air Force, Wright Air Development Center, 1951., 1951), also by Theodore H. H. Pian, Hua Lin, and Wright Air Development Center (page images at HathiTrust)
- Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory: Effect of structural flexibiligy on aircraft loading. Part III, Maneuvering load dynamic overstress (Wright-Patterson Air Force Base, Ohio : United States, Air Force, Air Materiel Command, 1951., 1951), also by Gabriel Isakson, Norman P. Hobbs, and United States. Air Force. Air Matériel Command (page images at HathiTrust)
- Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory: Effect of structural flexibiligy on aircraft loading. Part IV, Horizontal tail maneuvering loads (Wright-Patterson Air Force Base, Ohio : United States, Air Force, Air Materiel Command, 1951., 1951), also by Gabriel Isakson, Claude Brenner, and United States. Air Force. Air Matériel Command (page images at HathiTrust)
- Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory: Effect of structural flexibiligy on aircraft loading. Part IX, Lift and moment growths on a swept, tapered, rigid wing unpon entering a gust (Wright-Patterson Air Force Base, Ohio : United States, Air Force, Wright Air Development Center, 1953., 1953), also by F. O. Carta, Hua Lin, Theodore H. H. Pian, and Wright Air Development Center (page images at HathiTrust)
- Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory: Effect of structural flexibiligy on aircraft loading. Part V, Rapid estimation of some effects of aeroelasticity on airload distribution at an abrupt aileron distribution (Wright-Patterson Air Force Base, Ohio : United States, Air Force, Wright Air Development Center, 1952., 1952), also by Theodore H. H. Pian, Hua Lin, and Wright Air Development Center (page images at HathiTrust)
- Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory: Effect of structural flexibiligy on aircraft loading. Part VI, An approximate method for determining spanwise airload distribution over an elastic wing in subsonic flow (Wright-Patterson Air Force Base, Ohio : United States, Air Force, Wright Air Development Center, 1952., 1952), also by Hua Lin, Theodore H. H. Pian, and Wright Air Development Center (page images at HathiTrust)
- Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory: Effect of structural flexibiligy on aircraft loading. Part VII, A graphical method for determining the dynamic load of a nonlinear two-degrees-of-freedom system (Wright-Patterson Air Force Base, Ohio : United States, Air Force, Wright Air Development Center, 1953., 1953), also by Hua Lin, Theodore H. H. Pian, and Wright Air Development Center (page images at HathiTrust)
- Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory: Effect of structural flexibiligy on aircraft loading. Part VIII, Symmetric airload distribution over a thin elastic delta wing with subsonic leading edge at supersonic speed (Wright-Patterson Air Force Base, Ohio : United States, Air Force, Wright Air Development Center, 1953., 1953), also by Hua Lin, Theodore H. H. Pian, and Wright Air Development Center (page images at HathiTrust)
- Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory: Effect of structural flexibiligy on aircraft loading. Part XI, A general parametric study of maneuvering horizontal tail loads on a flexible airplane (Wright-Patterson Air Force Base, Ohio : United States, Air Force, Wright Air Development Center, 1953., 1953), also by K. A. Foss and Wright Air Development Center (page images at HathiTrust)
- Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory: Effect of structural flexibiligy on aircraft loading. Part XII, The gust response of a sweptback tapered wing including bending flexibility (Wright-Patterson Air Force Base, Ohio : United States, Air Force, Wright Air Development Center, 1953., 1953), also by A. Codik, Theodore H. H. Pian, Hua Lin, and Wright Air Development Center (page images at HathiTrust)
- Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory: Effect of structural flexibiligy on aircraft loading. Part XIII, Vertical tail maneuvering loads without banking degree of freedom (Wright-Patterson Air Force Base, Ohio : United States, Air Force, Wright Air Development Center, 1953., 1953), also by J. F. McCarthy, A. A. Kirsch, and Wright Air Development Center (page images at HathiTrust)
- Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory: Effect of structural flexibiligy on aircraft loading. Part XIV, An analogue study of horizontal tail maneuvering loads at various speeds for a typical bomber (Wright-Patterson Air Force Base, Ohio : United States, Air Force, Wright Air Development Center, 1954., 1954), also by S. J. Engel, J. F. McCarthy, and Wright Air Development Center (page images at HathiTrust)
- Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory: Effect of structural flexibiligy on aircraft loading. Part XIX, A parametric study of the gust response of swept wing airplanes including a wing-bending degree of freedom (Wright-Patterson Air Force Base, Ohio : United States, Air Force, Wright Air Development Center, 1954., 1954), also by K. A. Foss, Theodore H. H. Pian, Sternlight D., and Wright Air Development Center (page images at HathiTrust)
- Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory: Effect of structural flexibiligy on aircraft loading. Part XVI, Estimation of the dynamic overstress in straight wing airplanes (Wright-Patterson Air Force Base, Ohio : United States, Air Force, Wright Air Development Center, 1954., 1954), also by Theodore H. H. Pian, P. H. Winter, and Wright Air Development Center (page images at HathiTrust)
- Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory: Effect of structural flexibiligy on aircraft loading. Part XVIII, Vertical tail maneuvering loads with banking degrees of freedom (Wright-Patterson Air Force Base, Ohio : United States, Air Force, Wright Air Development Center, 1954., 1954), also by A. A. Kirsch, J. F. McCarthy, and Wright Air Development Center (page images at HathiTrust)
- Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory: The effects of structural elasticity on aircraft control systems (Wright Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1956., 1956), also by Vincent William Howard, United States. Air Force. Air Research and Development Command, and Wright Air Development Center (page images at HathiTrust)
- Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory: Further studies on high-speed unsteady flow (Wright-Patterson Air Force Systems Base, Ohio : Flight Dynamics Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), also by Garabed Zartarian, Harry Sauerwein, and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
- Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory: A study of matrix analysis methods for inelastic structures. Project no. 1467, Task no. 146701, prepared under Contract no. AF 33 (657)-8717 by Massachusetts Institute of Technology, Aeroelastic and Structures Research Laboratory. (AF Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, 1963), also by John H. Percy, D. K. Navaratna, and William A. Loden (page images at HathiTrust)
- Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory: Theoretical and experimental studies on airloads related to hypersonic aeroelastic problems of general slender pointed configurations (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1961., 1961), also by Garabed Zartarian, Pao Tan Hsu, United States. Air Force. Systems Command. Aeronautical Systems Division, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
- Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory: Transient and nonlinear effects on high speed, vibratory thermoelastic instability phenomena. Part I, Theoretical considerations (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Air Research and Development Command, U.S. Air Force, 1960., 1960), also by Eugene J. Brunelle, United States. Air Force. Air Research and Development Command, and United States. Wright Air Development Division (page images at HathiTrust; US access only)
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