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Gust loads

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• Aerodynamic load
• Atmospheric turbulence
• Wind-pressure

• Gust loads -- Computer programs
• Gust loads -- Computer simulation
• Gust loads -- Mathematical models
• Gust loads -- Measurement
• Gust loads -- Measurment
• Gust loads -- Meaurements
• Climatology -- Gust loads

• Turbulence statistics for design of wind turbine generators (U.S. Dept. of Commerce, National Oceanic and Atmospheric Administration, Environmental Research Laboratories, 1981), by J. C. Kaimal, D. E. Wolfe, J. E. Gaynor, United States. Dept. of Energy, Wave Propagation Laboratory, and Environmental Research Laboratories (U.S.) (page images at HathiTrust)
• Effects of gust velocity spatial distributions on lateral-directional response of a VTOL aircraft (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Directorate of Laboratories, Air Force Systems Command, 1967., 1967), by Robert L. Swaim, Alonzo J. Connors, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Total energy-rate feedback for automatic glide-slope tracking during wind-shear penetration (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by Christine M. Belcastro, Aaron J. Ostroff, and Langley Research Center (page images at HathiTrust)
• Dynamic wind-tunnel tests of an aeromechanical gust-alleviation system using several different combinations of control surfaces (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Eric C. Stewart, Robert V. Doggett, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Gust generator for a supersonic wind tunnel (National Aeronautics and Space Administration ;, 1974), by Bobby W. Sanders, John A. Webb, Allan R. Bishop, and Lewis Research Center (page images at HathiTrust)
• Wind-tunnel survey of an oscillating flow field for application to model helicopter rotor testing (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Paul H. Mirick, William T. Yeager, M-Nabil H. Hamouda, United States. Army Aerostructures Directorate, and Langley Research Center (page images at HathiTrust)
• Some properties of a five-parameter bivariate probability distribution (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by J. D. Tubbs, Orvel E. Smith, D. W. Brewer, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and George C. Marshall Space Flight Center (page images at HathiTrust)
• Application of active controls technology to the NASA JetStar airplane (National Aeronautics and Space Administration ;, 1975), by R. H. Lange, Flight Research Center (U.S.), and Lockheed-Georgia Company (page images at HathiTrust)
• Cross-spectral functions based on von Karman's spectral equation (National Aeronautics and Space Administration ;, 1972), by John C. Houbolt, Asim Sen, Langley Research Center, and Aeronautical Research Associates of Princeton (page images at HathiTrust)
• An analytical study of the reponse of a constant-attitude aircraft to atmospheric turbulence (National Aeronautics and Space Administration ;, 1973), by Frederick O. Smetana, Ronald K. Carden, Langley Research Center, and North Carolina State University (page images at HathiTrust)
• Active Control for the Total-In-Flight Simulator (ACTIFS) (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), by E. G. Rynaski, N. Weingarten, D. Andrisanti, Calspan Corporation, Langley Research Center, United States. Air Force. Systems Command, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Dynamic response of airplanes to atmospheric turbulence including flight data on input and response (National Aeronautics and Space Administration, 1964), by John C. Houbolt, Kermit G. Pratt, Roy Steiner, and Langley Research Center (page images at HathiTrust)
• High altitude gust acceleration environment as experienced by a supersonic airplane (National Aeronautics and Space Administration ;, 1975), by L. J. Ehernberger, Betty J. Love, and Flight Research Center (U.S.) (page images at HathiTrust)
• Summary of VGH and V-G data obtained from piston-engine transport airplanes from 1947 to 1958 (National Aeronautics and Space Administration, 1959), by Walter G. Walker, Martin R. Copp, and Langley Research Center (page images at HathiTrust)
• An analytical study and wind-tunnel tests of an aeromechanical gust-alleviation system for a light airplane (National Aeronautics and Space Administration ;, 1976), by Eric C. Stewart (page images at HathiTrust)
• Computed lateral rate and acceleration power spectral response of conventional and STOL airplanes to atmospheric turbulence (National Aeronautics and Space Administration ;, 1975), by Jacob H. Lichtenstein and Langley Research Center (page images at HathiTrust)
• A method for the analysis of nonlinearities in aircraft dynamic response to atmospheric turbulence. (National Aeronautics and Space Administration ;, 1976), by Kenneth Sidwell (page images at HathiTrust)
• Recent advances in aerodynamic energy concept for flutter suppression and gust alleviation using active controls. (National Aeronautics and Space Administration ;, 1977), by E. Nissim, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Computed lateral power spectral density response of conventional and STOL airplanes to random atmospheric turbulence (National Aeronautics and Space Administration ;, 1974), by Jacob H. Lichtenstein and Langley Research Center (page images at HathiTrust)
• Analytical study of the performance of a gust alleviation system with a vane sensor (National Aeronautics and Space Administration ;, 1974), by Waldo I. Oehman and Langley Research Center (page images at HathiTrust)
• Gust alleviation for a STOL transport by using elevator, spoilers, and flaps (National Aeronautics and Space Administration ;, 1974), by Frederick J. Lallman and Langley Research Center (page images at HathiTrust)
• NASA TN D-6126 (National Aeronautics and Space Administration :, 1971), by L. Keith Barker, Gene W. Sparrow, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analytical study of the performance of a gust alleviation system for a STOL airplane (National Aeronautics and Space Administration ;, 1973), by Waldo I. Oehman and Langley Research Center (page images at HathiTrust)
• Initial experimental investigation of the aerodynamic load on the wing of a model caused by a blast-induced gust that increases the angle of attack into the stall region (National Advisory Committee for Aeronautics, 1955), by Harold B. Pierce, Thomas D. Reisert, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• An analysis of the relation between horizontal temperature variations and maximum effective gust velocities in thunderstorms (National Advisory Committee for Aeronautics, 1949), by H. Press, J. K. Thompson, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• The Application of the statistical theory of extreme values to gust-load problems (National Advisory Committee for Aeronautics, 1949), by Harry Press and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Gust-tunnel investigation of a flexible-wing model with semichord line swept back 45° (National Advisory Committee for Aeronautics, 1949), by Thomas D. Reisert and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• A recurrence matrix solution for the dynamic response of aircraft in gusts (National Advisory Committee for Aeronautics, 1950), by John C. Houbolt and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lift developed on unrestrained rectangular wings entering gusts at subsonic and supersonic speeds (National Advisory Committee for Aeronautics, 1953), by Harvard Lomax and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Correlation of calculation and flight studies of the effect of wing flexibility on structural response due to gusts (National Advisory Committee for Aeronautics, 1953), by John C. Houbolt and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Estimates of probability distribution of root-mean-square gust velocity of atmospheric turbulence from operational gust-load data by random-process theory (National Advisory Committee for Aeronautics, 1955), by Harry Press, Ivan Hadlock, May T. Meadows, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Extreme wind speeds, gustiness, and variations with height for MIL-STD 210B (Air Force Cambridge Research Laboratories, Air Force Systems Command, United States Air Force, 1973), by Norman Sissenwine, Irving I. Gringorten, D. D. Grantham, Paul Tattelman, and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• Numerical simulation of thunderstorm gust fronts (Hanscom AFB, Massachusetts : Air Force Geophysics Laboratory, Air Force Systems Command, United States Air Force, 1983., 1983), by Keith L. Seitter and U.S. Air Force Geophysics Laboratory. Atmospheric Sciences Division (page images at HathiTrust)
• Windspeed profile, windshear, and gusts for design of guidance systems for vertical rising air vehicles (Cambridge, Massachusetts : Special Projects Laboratory, Geophysics Research Directorate, Air Force Cambridge Research Center, Air Research and Development Command, [1954], 1954), by Norman Sissenwine and Air Force Cambridge Research Center (U.S.). Geophysics Research Directorate (page images at HathiTrust)
• Detection of gust fronts using surface sensors (Wave Propagation Laboratory, Environmental Research Laboratories, 1977), by A. J. Bedard and Wave Propagation Laboratory (page images at HathiTrust)
• Efficient dealiasing of doppler velocities using local environmental constraints (Federal Aviation Administration, Advanced System Acquisition Service ;, 1989), by Michael D. Ellis, Steven D. Smith, National Severe Storms Laboratory, and United States. Federal Aviation Administration. Advanced System Acquisition Service (page images at HathiTrust)
• Development and testing of the gust front algorithm (Federal Aviation Administration, Program Engineering Service ;, 1987), by Arthur Witt, Steven D. Smith, National Severe Storms Laboratory, and United States. Federal Aviation Administration. Program Engineering Service (page images at HathiTrust)
• 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), by Arthur L. Jones, 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)
• 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), by Arthur L. Jones, 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)
• Gust loading of rigid and flexible aircraft in continuous atmospheric turbulence (Wright Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1958., 1958), by Kenneth A. Foss, Warren L. McCabe, United States. Air Force. Air Research and Development Command, and Wright Air Development Center (page images at HathiTrust)
• Low Altitude Atmospheric Turbulence LO-LOCAT phase III interim report. Volume I, Data acquisition and analysis (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1969., 1969), by K. R. Monson, R. H. Mielke, G. W. Jones, Air Force Flight Dynamics Laboratory (U.S.), and United States. Air Force. Systems Command (page images at HathiTrust)
• Investigation of the effects of gusts on V/STOL craft in transition and hover (Wright-Patterson Air Force Base : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1968., 1968), by Grant Brandford Skelton, Air Force Flight Dynamics Laboratory (U.S.), and Honeywell Inc. Systems and Research Division (page images at HathiTrust)
• B-66B low level gust study. Volume XI, Crew Comments. Part 2, Flights G-54-G115 (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Flight Dynamics Laboratory, Air Research and Development Command, United States Air Force, 1961., 1961), by Air Force Flight Dynamics Laboratory (U.S.), United States. Wright Air Development Division, United States. Air Force. Air Research and Development Command, and Douglas Aircraft Company (page images at HathiTrust)

• A computer program to obtain time-correlated gust loads for nonlinear aircraft using the matched-filter-based method (Federal Aviation Administration Technical Center ;, 1994), by Robert C. Scott, Boyd Perry, Anthony S. Pototzky, Langley Research Center. Aeroelasticity Branch, and Federal Aviation Administration Technical Center (U.S.) (page images at HathiTrust)

• The passage of an infinite swept airfoil through an oblique gust (National Aeronautics and Space Administration ;, 1974), by John J. Adamczyk, Langley Research Center, and United Aircraft Corporation. Research Laboratories (page images at HathiTrust)

• Development of a linearized unsteady aerodynamic analysis for cascade gust response predictions (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Joseph M. Verdon, Kenneth C. Hall, Lewis Research Center, and United Technologies Research Center (page images at HathiTrust)
• Determination of critical nondimensional parameters in aircraft dynamic response to random input (National Aeronautics and Space Administration ;, 1974), by Stanley E. Hillard, Maurice M. Sevik, George C. Marshall Space Flight Center, and Pennsylvania State University (page images at HathiTrust)
• Kahuku kite wind study : III. Turbulence analysis (Dept. of Meteorology, University of Hawaii, 1982), by P. Anders Daniels and University of Hawaii at Manoa. Dept. of Meteorology (page images at HathiTrust; US access only)
• Reduction of incremental load factor acceleration data to gust statistics (FAA Technical Center ;, 1994), by J. B. de Jonge, Nationaal Lucht- en Ruimtevaartlaboratorium (Netherlands), Federal Aviation Administration Technical Center (U.S.), and Netherlands. Rijksluchtvaartdienst (page images at HathiTrust)
• Reanalysis of European flight loads data (FAA Technical Center ;, 1994), by J. B. de Jonge, P. A. van Gelder, P. A. Hol, Nationaal Lucht- en Ruimtevaartlaboratorium (Netherlands), and Federal Aviation Administration Technical Center (U.S.) (page images at HathiTrust)
• Statistical loads data for Boeing 737-400 aircraft in commercial operations (Federal Aviation Administration, Office of Aviation Research ;, 1998), by John Rustenburg, Daniel O. Tipps, Donal Skinn, University of Dayton. Research Institute, and United States. Federal Aviation Administration. Office of Aviation Research (page images at HathiTrust)

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