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Equations of motion

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• Mechanics

• Lagrange equations

• Equations of motion -- Computer programs
• Equations of motion -- Mathematical models
• Equations of motion -- Research

• Motion equations

• Analysis of flow through a sphere : first report (Oakridge National Laboratory, 1952), by D. H. Fax, George F. Wislicenus, S. C. Traugott, U.S. Atomic Energy Commission, and Oak Ridge National Laboratory. Reactor Experimental Engineering Division (page images at HathiTrust)
• Space station rotational equations of motion (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by Mario H. Rheinfurth, Stanley N. Carroll, and George C. Marshall Space Flight Center (page images at HathiTrust)
• Technique to eliminate computational instability in multibody simulations employing the Lagrange multiplier (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by G. Watts and George C. Marshall Space Flight Center. Structures and Dynamics Laboratory (page images at HathiTrust)
• Computer mechanization of reentry equations with four degrees of freedom (National Aeronautics and Space Administration ;, 1968), by R. M. Howe, University of Michigan, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Theoretical study of vortex shedding from bodies of revolution undergoing coning motion (National Aeronautics and Space Administration ;, 1969), by Gary D. Kuhn, Jack N. Nielsen, Selden B. Spangler, Ames Research Center, and Inc Nielsen Engineering & Research (page images at HathiTrust)
• Transient vibration analysis of linear systems using transition matrices (National Aeronautics and Space Administration ;, 1968), by Anthony Craggs, University of Southampton, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• The transient response of coupled acousto-mechanical systems (National Aeronautics and Space Administration ;, 1969), by A. Craggs, Langley Research Center, and University of Southampton (page images at HathiTrust)
• A lattice model for composite materials (National Aeronautics and Space Administration ;, 1969), by Theodore R. Tauchert, A. Cemal Eringen, T. Y. Chang, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Numerical calculations of viscous compressible fluid flow around a stationary cylinder (National Aeronautics and Space Administration ;, 1970), by John G. Trulio, Leonard Walitt, George C. Marshall Space Flight Center, and inc Applied Theory (page images at HathiTrust)
• Formulation on statistical trajectory estimation programs (National Aeronautics and Space Administration ;, 1970), by William E. Wagner, Arno C. Serold, Langley Research Center, and Martin Marietta Corporation (page images at HathiTrust)
• Calculation of turbulent boundary layers with heat transfer and pressure gradient utilizing a compressibility transformation. Part II, Constant property turbulent boundary layer flow with simultaneous mass transfer and pressure gradient (National Aeronautics and Space Administration ;, 1972), by J. Boccio, C. Economos, Langley Research Center, and Nassau County General Applied Science Laboratories (Westbury (page images at HathiTrust)
• A method for analyzing the aeroelastic stability of a helicopter rotor in forward flight (National Aeronautics and Space Administration ;, 1969), by Peter Crimi, Applied Science Associates, and Langley Research Center (page images at HathiTrust)
• New formulation and equilibrium orientations deduced from an integral of motion (National Aeronautics and Space Administration, 1965), by Raynor L. Duncombe, I. Michelson, Illinois Institute of Technology, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Solution of the exact equations for three-dimensional atmospheric entry using directly matched asymptotic expansions (U.S. National Aeronautics and Space Administration, Langley Research Center ;, 1976), by Adolf Busemann, Robert D. Culp, Nguyen X. Vinh, University of Colorado, and Langley Research Center (page images at HathiTrust)
• Aeorelastic analysis for helicopter rotor blades with time-variable, nonlinear structural twist and multiple structural redundancy-mathematical derivation and program user's manual (National Aeronautics and Space Administration ;, 1976), by Richard L. Bielawa, United Technologies Research Center, United States National Aeronautics and Space Administration, Langley Research Center, and U.S. Army Air Mobility Research and Development Laboratory (page images at HathiTrust)
• Some aspects of essentially nonoscillatory (ENO) formulations for the Euler equations (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Sukumar R. Chakravarthy, Langley Research Center, and Rockwell International. Science Center (page images at HathiTrust)
• NASA TR R-228 (National Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Department of Commerce, Washington, D.C. 20230], 1966), by Charlie M. Jackson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Nonlinear equations of motion for the elastic bending and torsion of twisted nonuniform rotor blades (National Aeronautics and Space Administration ;, 1974), by Dewey H. Hodges, E. H. Dowell, U.S. Army Air Mobility Research and Development Laboratory, and Ames Research Center (page images at HathiTrust)
• NASA TN D-6468 (National Aeronautics and Space Administration :, 1971), by Dallas G. Denery, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-6069 (National Aeronautics and Space Administration ;, 1970), by Harvey Walden, Goddard Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Numerical integration of orbits in multirevolution steps. (National Aeronautics and Space Administration :, 1970), by C. E. Velez, Goddard Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• The effects of a nonrigidly supported ballast on the dynamics of a slender body descending through the atmosphere. (National Aeronautics and Space Administration :, 1970), by Gerald N. Malcolm, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Spherical balloon response to three-dimensional time-dependent flows (National Aeronautics and Space Administration ;, 1972), by George H. Fichtl and George C. Marshall Space Flight Center (page images at HathiTrust)
• Effect of eccentricity of the lunar orbit, oblateness of the Earth, and solar gravitational field on lunar trajectories (National Aeronautics and Space Administration, 1960), by William H. Michael, Robert H. Tolson, and Langley Research Center (page images at HathiTrust)
• Analysis of one-dimensional ion rocket with grid neutralization (National Aeronautics and Space Administration, 1960), by Harold Mirels, Burt M. Rosenbaum, and Lewis Research Center (page images at HathiTrust)
• NASA TN D-4622 (National Aeronautics and Space Administration :, 1968), by Rowland E. Burns, George C. Marshall Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• A qualitative study of the complete set of solutions of the differential equation of motion of a test particle in the equatorial plane of the Kerr gravitational field (National Aeronautics and Space Administration, 1973), by Harry E. Montgomery and F. K. Chan (page images at HathiTrust)
• Investigation of a clamshell roll-out ejection concept (National Aeronautics and Space Administration :, 1971), by Lawrence F. Hatakeyama, Goddard Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analysis of the dynamic lateral stability of a delta-wing airplane with frequency-dependent stability derivatives (National Aeronautics and Space Administration, 1959), by Albert E. Brown, Albert A. Schy, and Langley Research Center (page images at HathiTrust)
• Electron dynamics in a plasma focus (National Aeronautics and Space Administration ;, 1977), by Frank Hohl, Patricia A. Winters, S. Peter Gary, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• On a class of exact solutions of the equations of motion of a viscous fluid (NACA, 1953), by V. I. Yatseyev and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Measurement of the longitudinal moment of inertia of a flexible airplane (National Advisory Committee for Aeronautics, 1956), by Henry Ambrose Cole, Frances L. Bennion, United States National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
• Experimental and predicted lateral-directional dynamic-response characteristics of a large flexible 35 degree swept-wing airplane at an altitude of 35,000 feet (National Advisory Committee for Aeronautics, 1956), by Stuart C. Brown, Euclid C. Holleman, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Differential equations of motion for combined flapwise bending, chordwise bending, and torsion of twisted nonuniform rotor blades (National Advisory Committee for Aeronautics, 1957), by John C. Houbolt, George W. Brooks, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Stability of a cable-moored airship (Sandia Corporation ;, 1959), by M. D. Bennett, U.S. Atomic Energy Commission, and Sandia Corporation (page images at HathiTrust; US access only)
• Impulsive loading of a circular disk (Sandia Corporation ;, 1961), by W. B. Murfin and Sandia Corporation (page images at HathiTrust)
• Impulsive loading of cylindrical shells (Sandia Corporation ;, 1961), by W. B. Murfin and Sandia Corporation (page images at HathiTrust)
• Couette flow at intermediate pressures (Union Carbide Nuclear Company, Oak Ridge Gaseous Diffusion Plant, 1958), by Wendell C. DeMarcus, Oak Ridge Gaseous Diffusion Plant, Union Carbide Nuclear Company, and U.S. Atomic Energy Commission (page images at HathiTrust)
• An exact re-statement of the equations of motion of a rigid projectile for use with modern computing machinery (Aberdeen, Maryland : Aberdeen Proving Ground, 1954., 1954), by Serge J. Zaroodny, U.S. Army Ballistic Research Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Chapman-Kirk reduction of free-flight range data to obtain nonlinear aerodynamic coefficients (Aberdeen, Maryland : Aberdeen Proving Ground, 1973., 1973), by Robert H. Whyte, James W. Bradley, Angela Jeung, U.S. Army Ballistic Research Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• The dynamical effect of inertial waves on the free flight motion of a body containing several eccentrically located, liquid-filled cylinders (Aberdeen Proving Ground, Maryland : U.S. Army Aberdeen Research and Development Center, Ballistic Research Laboratories, 1971., 1971), by Wayman Eugene Scott and U.S. Army Ballistic Research Laboratory (page images at HathiTrust)
• Expansion of tables II and III of National Adviosry Committee for Aeronautics technical note no. 1428 (Aberdeen Proving Ground, Maryland : Ballistic Research Laboratories, 1951., 1951), by U.S. Army Ballistic Research Laboratory (page images at HathiTrust)
• Deceleration and vertical motion of a gas puff released into the upper atmosphere (Air Force Cambridge Research Laboratories, Air Force Systems Command, United States Air Force, 1973), by Milton M. Klein and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• Thermally stratified compressible fluid motion on a rotating sphere with gravitation (Air Force Cambridge Research Laboratories, Air Force Systems Command, United States Air Force, 1973), by Edmond M. Dewan and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• An exact solution for the rotation of the atmosphere about the spheroidal earth (Air Force Cambridge Research Laboratories, Air Force Systems Command, United States Air Force, 1973), by Harry E. Moses and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• Propagation of internal gravity waves in a medium of weak random vertical shear (Air Force Cambridge Research Laboratories, Air Force Systems Command, United States Air Force, 1973), by J. M. Forbes and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• A dynamic model of the general theory of electric machines (Oak Ridge, Tennessee : U.S. Atomic Energy Commission, Technical Information Service, 1953., 1953), by A. V. Gaponov-Grekhov, U.S. Atomic Energy Commission, and National Science Foundation (U.S.) (page images at HathiTrust)
• Equations of motion and field equations in the five-dimensional unitary theory of relativity (Oak Ridge, Tennessee : U.S. Atomic Energy Commission, Technical Information Service, 1953., 1953), by Roman S. Ingarden, U.S. Atomic Energy Commission, and National Science Foundation (U.S.) (page images at HathiTrust)
• A Numerical Model for Investigation of Ozone Transport in the Atmosphere (L.G. Hanscom Field, Bedford, Massachusetts : Air Force Cambridge Research Laboratories, Office of Aerospace Research, United States Air Force, 1971., 1971), by Louis Berkofsky, Shoshana Gyoeri, and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• The motion of trails through fluids with constant velocity shear (L.G. Hanscom Field, Bedford, Massachusetts : Air Force Cambridge Research Laboratories, Office of Aerospace Research, United States Air Force, 1971., 1971), by Harry E. Moses and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• Frequency model for the GI-T1-B single degree of freedom rate integrating gyroscope (L.G. Hanscom Field, Bedford, Massachusetts : Air Force Cambridge Research Laboratories, Air Force Systems Command, United States Air Force, 1971., 1971), by Thomas S. Rhoades and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• On the first and a related adiabatic invariant with a force in the direction of the velocity (Hanscom AFB, Massachusetts : Air Force Geophysics Laboratory, Air Force Systems Command, United States Air Force, 1980., 1980), by Charles W. Dubs and U.S. Air Force Geophysics Laboratory (page images at HathiTrust)
• A simple exact solution for the motion of the atmosphere about the rotating earth and application to the rotation of the atmosphere (L.G. Hanscom Field, Bedford, Massachusetts : Air Force Cambridge Research Laboratories, Office of Aerospace Research, United States Air Force, 1972., 1972), by Harry E. Moses and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• Numerical model of the equatorial electrojet (L.G. Hanscom Field, Bedford, Massachusetts : Air Force Cambridge Research Laboratories, Office of Aerospace Research, United States Air Force, 1972., 1972), by Arthur D. Richmond and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• A mathematical model of the evolution of radiation fog (L.G. Hanscom FIeld, Bedford, Massachusetts : Air Force Cambridge Research Laboratories, Air Force Systems Command, United States Air Force, 1972., 1972), by I. M. Zakharova and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• An exploratory theoretical investigation of the effect of longitudinal surface curvature on the turbulent boundary layer (White Oak, Maryland : United States Naval Ordnance Laboratory, 1969., 1969), by Neal Tetervin and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Numerical calculation of the response of coastal waters to storm systems : with application to Hurricane Camille of August 17-22, 1969 (Coastal and Oceanographic Engineering Laboratory, University of Florida, 1972), by Bryan Rowell Pearce (page images at HathiTrust)
• Computation of hypersonic axially symmetric flow at low Mach numbers (New York, New York : AEC Computing and Applied Mathematics Center, Courant Institute of Mathematical Sciences, New York University, 1968, 1968), by David Korn and Courant Institute of Mathematical Sciences (page images at HathiTrust)
• Study of the dynamics of train motion with special reference to the theory and the applications of speed-time, distance-time and speed-distance curves (1917), by Sentaro Sekine (page images at HathiTrust; US access only)
• An Investigation of the damping in pitch characteristics of a ten degree cone (Silver Spring, Maryland : Naval Surface Weapons Center, White Oak Laboratory, 1975., 1975), by A. M. Morrison, W. R. Lawrence, J. E. Holmes, and Naval Surface Weapons Center. White Oak Laboratory (page images at HathiTrust)
• Handbook of blunt-body aerodynamics: volume 1 - static stability. (Silver Spring, Maryland : Naval Ordnance Laboratory, White Oak, 1973., 1973), by John A. Darling and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Rayleigh's problem in hydromagnetics : impulsive motion of a pole-piece ([Washington, D.C.] : [United States Air Force, Office of Scientific Research], 1958., 1958), by G. S. S. Ludford, United States. Air Force. Office of Scientific Research, and College Park. Institute for Fluid Dynamics and Applied Mathematics University of Maryland (page images at HathiTrust)
• Transmission line models of magnon-phonon modes in ferrites. Part I. Uncoupled modes (L. G. Hansom Field, Bedford, Massachusetts : Air Force Cambridge Research Laboratories, Office of Aerospace Research, United States Air Force, 1966., 1966), by James C. Sethares and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• Transmission line models of Magnon-Phonon modes in ferrites. Part II. Coupled modes (L. G. Hansom Field, Bedford, Massachusetts : Air Force Cambridge Research Laboratories, Office of Aerospace Research, United States Air Force, 1967., 1967), by James C. Sethares and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• Eigenfunctions of the curl operator, rotationally invariant Helmholtz theorem, and applications to electromagnetic theory and fluid dynamics (L.G. Hansom Field, Bedford, Massachusetts : Air Force Cambridge Research Laboratories, Office of Aerospace Research, United States Air Force, 1970., 1970), by H. E. Moses and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• Estimation of flying qualities of piloted airplanes (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems command, 1966., 1966), by Robert J. Woodcock, D. E. Drake, Wright-Patterson Air Force Base (Ohio), Douglas Aircraft Company, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Development of weapon delivery models and analysis programs. Volume I, System modeling and performance optimization (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1972., 1972), by A. Ferit Konar, Honeywell Inc. Systems and Research Division, Air Force Flight Dynamics Laboratory (U.S.), and Armament Delivery Analysis Programming System (ADAPS) (page images at HathiTrust)
• Velocity distribution in the wake of bodies of revolution based on drag coefficient (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1963., 1963), by Helmut G. Heinrich, Donald J. Eckstrom, Wright-Patterson Air Force Base (Ohio), United States. Air Force. Systems Command. Aeronautical Systems Division, and University of Minnesota. Department of Aerospace Engineering and Mechanics (page images at HathiTrust)
• Exact vorticity solutions of the incompressible Navier-Stokes equations (L.G. Hansom Field, Bedford, Massachusetts : Air Force Cambridge Research Laboratories, Office of Aerospace Research, United States Air Force, 1970., 1970), by Harry E. Moses and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• Development of weapon delivery models and analysis programs. Volume II, Documentation of the Armament Delivery Analysis Programming System (ADAPS) (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1972., 1972), by A. Ferit Konar, Michael D. Ward, Honeywell Inc. Systems and Research Division, Air Force Flight Dynamics Laboratory (U.S.), and Armament Delivery Analysis Programming System (ADAPS) (page images at HathiTrust)
• Development of weapon delivery models and analysis programs. Volume III, Testing and demonstration of the Armament Delivery Analysis Programming System (ADAPS) (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1972., 1972), by A. Ferit Konar, Michael D. Ward, Honeywell Inc. Systems and Research Division, Air Force Flight Dynamics Laboratory (U.S.), and Armament Delivery Analysis Programming System (ADAPS) (page images at HathiTrust)
• Compensation of interpolation by linear filter (L.G. Hansom Field, Bedford, Massachusetts : Air Force Cambridge Research Laboratories, Office of Aerospace Research, United States Air Force, 1971., 1971), by Ralph Shapiro and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• Some solutions of the diffusion equation for an expanding gas cloud in a constant shear flow (L.G. Hansom Field, Bedford, Massachusetts : Air Force Cambridge Research Laboratories, Office of Aerospace Research, United States Air Force, 1971., 1971), by Antonio F. Quesada and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• Vertical shear modes in inertial waves on a rotating earth (L.G. Hansom Field, Bedford, Massachusetts : Air Force Cambridge Research Laboratories, Office of Aerospace Research, United States Air Force, 1970., 1970), by Harry E. Moses and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• Analysis of propagation in space-time modulated media using many-space scale perturbation theory (L.G. Hansom Field, Bedford, Massachusetts : Air Force Cambridge Research Laboratories, Office of Aerospace Research, United States Air Force, 1972., 1972), by Ronald L. Fante and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• Unsteady aerodynamic pressures in transonic flow (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1971., 1971), by L. V. Andrew, Air Force Flight Dynamics Laboratory (U.S.), and North American Rockwell Corporation (page images at HathiTrust)
• Non-linear effects in the longitudinal dynamics of a lifting vehicle in a circular orbit (Toronto, Canada : University of Toronto, Institute of Aerophysics, 1960., 1961), by R. S. Rangi, University of Toronto. Institute of Aerophysics, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• The use of a multi-degree-of-freedom dual balance system to measure cross and cross-coupling derivatives (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1982., 1982), by D. R. Haberman, Calspan Field Services, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
• User's manual : extended capability magnus rotor and ballistic body 6-DOF trajectory program (Eglin Air Force Base, Florida : Air Force Armament Laboratory, Air Force Systems Command, United States Air Force, 1970., 1970), by James E. Brunk, United States. Air Force. Systems Command, and Air Force Armament Laboratory (page images at HathiTrust)
• An analytic investigation of accuracy requirements for onboard instrumentation and film data for dynamically scaled wind tunnel drop models (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1997., 1997), by K. S. Keen, R. L. Arterbury, C. H. Morgret, Inc Sverdrup Technology, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
• Characteristic boundary conditions for ARO-1 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1983., 1983), by Karl R. Kneile, James L. Jacocks, Donald C. Todd, Calspan Field Services, Inc Sverdrup Technology, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
• Equations for store separation motion simulations and instrumented model data reduction (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1996., 1996), by K. S. Keen, Calspan Corporation, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
• A study of simulators for the lateral motions of an automobile (Cornell Aeronautical Laboratory, 1954), by A. G. Fonda and Cornell Aeronautical Laboratory (page images at HathiTrust; US access only)
• Flight simulation of orbital and reentry vehicles. Part 1. Development of equations of motion in six degrees of freedom (Wright-Patterson Air Force Base, Ohio : Aerospace Medical Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), by Gabriel Isakson, United States. Air Force. Systems Command. Aeronautical Systems Division, Aerospace Medical Laboratory (U.S.), and University of Michigan (page images at HathiTrust)
• Aircraft motion analysis (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), by J. A. Thelander, United States. Air Force. Systems Command, Air Force Flight Dynamics Laboratory (U.S.), and Douglas Aircraft Company (page images at HathiTrust)
• Missile dynamics equations for guidance and control modeling and analysis (Redstone Arsenal, Alabama : U.S. Army Missile Command, 1984., 1984), by Philip N. Jenkins, Redstone Arsenal (Ala.), and United States. Army. Missile Command (page images at HathiTrust)
• An Application of potential flow to slender bodies of revolution (China Lake, California : U.S. Naval Ordnance Laboratory, Underwater Ordnance Department, 1961., 1961), by Jack F. Reynolds and Calif.) Naval Ordnance Test Station (China Lake (page images at HathiTrust)
• Effect of horizontal and vertical side forces and moments on stability of a symmetric missile in ascending or descending flight (Aberdeen Proving Ground, Maryland : Ballistic Research Laboratory, 1979., 1979), by Charles H. Murphy and U.S. Army Ballistic Research Laboratory (page images at HathiTrust)
• Engineering analysis methods for linear time varying systems (Wright-Patterson Air Force Base, Ohio : Flight Control Laboratory, Aeronautical Systems Division, Air Force Systems Command, [1963], 1963), by Dunstan Graham, Harry Passmore, Walter Johnson, Eugene J. Brunelle, United States. Air Force. Systems Command. Aeronautical Systems Division, Wright-Patterson Air Force Base (Ohio), and Inc Systems Technology (page images at HathiTrust)
• Analytic solutions to the equations of motion of missiles having Six degrees of freedom (U) (White Oak, Maryland : United States Naval Ordance Laboratory, 1964., 1964), by W. E. DeGrafft and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• A Kinetic theory development of the equations of motion of a diatomic gas (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1986., 1986), by William Z. Strang, Air Force Wright Aeronautical Laboratories, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Solution of transient problems in free surface hydrodynamics (Washington, D. C. : Naval Research Laboratory, 1977., 1977), by M. J. Fritts, J. P. Boris, inc Science Applications, Naval Research Laboratory (U.S.), and United States. Office of Naval Research (page images at HathiTrust)
• A general theory and analysis of the dynamic stability of flexible-bodied missiles (Wright-Patterson Air Force Base, Ohio : Flight Control Laboratory, Aeronautical Systems DIvision, Air Force Systems Command, United States Air Force, 1962., 1962), by Robert L. Swaim and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• An analysis of fixed wing-proprotor interference for folding proprotor aircraft (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1973., 1973), by Carl G. Matthys, P. Y. Hsieh, Mukund M. Joglekar, Air Force Flight Dynamics Laboratory (U.S.), United States. Air Force. Systems Command, and Bell Helicopter Company (page images at HathiTrust)

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