Darcy's law -- Mathematical modelsSee also what's at your library, or elsewhere.
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Filed under: Darcy's law -- Mathematical models
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Filed under: Darcy's law- An equation for unsaturated flow based upon the Darcy equation and an analogy of the Poiseuille equation (U.S. Atomic Energy Commission, 1960), by P. P. Rowe, United States. National Bureau of Standards, United States. Department of Energy. Office of Fusion Energy, United States. National Bureau of Standards. Fracture and Deformation Division, U.S. Atomic Energy Commission, United States. Energy Research and Development Administration, Hanford Works, and Hanford Atomic Products Operation. Chemical Research and Development Operation (page images at HathiTrust)
- Validity of Darcy's law under transient conditions (U.S. Dept. of the Interior, U.S. Geological Survey ;, 1985), by Charles E. Mongan and Geological Survey (U.S.) (page images at HathiTrust)
Filed under: Fluid dynamics -- Mathematical models- On the formulation and numerical evaluation of a set of two-phase flow equations modelling the cool-down process. (For sale by the Superintendent of Documents, U.S. Govt. Print. Off., 1965), by Stephen Jarvis (page images at HathiTrust)
- Marangoni convection in a gravity-free silicon float zone (Carderock Division, Naval Surface Warfare Center, 1994), by Samuel Ohring, Hans J. Lugt, and Naval Surface Warfare Center (U.S.). Carderock Division (page images at HathiTrust)
- The turbulent mean-flow, Reynolds-stress, and heat-flux equations in mass-averaged dependent variables (Ames Research Center?, 1973), by Morris W. Rubesin (page images at HathiTrust)
- On the problem of liquid entrainment (Argonne National Laboratory, 1960), by Gordon C. K. Yeh, N. Zuber, U.S. Atomic Energy Commission, Argonne National Laboratory, and inc. Ramo-Wooldridge Division Thompson Ramo Wooldridge (page images at HathiTrust)
- Computer modeling of fluid flow during production and environmental restoration phases of in situ uranium leaching (U.S. Dept. of the Interior, Bureau of Mines, 1980), by R. D. Schmidt (page images at HathiTrust)
- Taylor's hydrodynamics of strong shocks applied to gases having small values of [gamma] -1 (Atomic Energy Commission, 1946), by J. Hirschfelder, U.S. Atomic Energy Commission, and Los Alamos Scientific Laboratory (page images at HathiTrust)
- Interactions of Tollmien-Schlichting waves and Dean vortices : comparison of direct numerical simulation and a weakly nonlinear theory (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), by Bart A. Singer, Thomas A. Zang, and Langley Research Center (page images at HathiTrust)
- Viscous-inviscid calculations of jet entrainment effects on the subsonic flow over nozzle afterbodies (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), by Richard G. Wilmoth, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- Numerical modeling of physical vapor transport in a vertical cylindrical ampoule, with and without gravity (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), by Timothy L. Miller and George C. Marshall Space Flight Center (page images at HathiTrust)
- Breakdown of the conservative potential equation (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), by M. D. Salas, Clyde R. Gumbert, and Langley Research Center (page images at HathiTrust)
- A critical evaluation of various turbulence models as applied to internal fluid flows (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985), by M. Nallasamy and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Solution of axisymmetric and two-dimensional inviscid flow over blunt bodies by the method of lines (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by H. Harris Hamilton, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- First derivatives of flow quantities behind two-dimensional, nonuniform supersonic flow over a convex corner (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by Christine M. Darden and Langley Research Center (page images at HathiTrust)
- Rainbow schlieren (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by Walton L. Howes and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Analysis of laminar flow between stationary and rotating disks with inflow (National Aeronautics and Space Administration ;, 1974), by Upendra S. Rohatgi, Eli Reshotko, Lewis Research Center, and Case Western Reserve University (page images at HathiTrust)
- Some problems of the calculation of three-dimensional boundary-layer flows on general configurations (National Aeronautics and Space Administration ;, 1973), by Tuncer Cebeci, Langley Research Center, and Douglas Aircraft Company (page images at HathiTrust)
- Mass diffusion in a self-confined rotating flow (National Aeronautics and Space Administration ;, 1972), by K. E. Torrance, Lewis Research Center, and Cornell University (page images at HathiTrust)
- Hyperbolic/parabolic development for the GIM-STAR code (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by L. W. Spradley, A. W. Ratliff, J. F. Stalnaker, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Computation of three-dimensional nozzle-exhaust flow fields with the GIM code (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by L. W. Spradley, M. L. Pearson, P. G. Anderson, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- An inventory of some force producers for use in marine vehicle control (David W. Taylor Naval Ship Research and Development Center, 1979), by Michael B. Wilson, Christian Von Kerczek, and David W. Taylor Naval Ship Research and Development Center (page images at HathiTrust)
- Two-dimensional hydrodynamic calculations (Los Alamos Scientific Laboratory of the University of California, 1959), by Francis H. Harlow, Robert E. Martin, David E. Harris, Donald O. Dickman, Los Alamos Scientific Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
- Theory of correspondence between fluid dymanics and particle-and-force models (Los Alamos Scientific Laboratory of the University of California, 1963), by Francis H. Harlow, Los Alamos Scientific Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
- The particle-and-force computing method for fluid dynamics (Los Alamos Scientific Laboratory of the University of California, 1961), by Francis H. Harlow, Billy D. Meixner, Los Alamos Scientific Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
- Equilibrium time for a square plants with one infinite reservoir (Union Carbide Nuclear Company, Oak Ridge Gaseous Diffusion Plant, 1961), by D. W. Burton, U.S. Atomic Energy Commission, Union Carbide Nuclear Company, and Oak Ridge Gaseous Diffusion Plant (page images at HathiTrust)
- Transient behavior of a square plant, separating a binary mixture, over an infinite reservoir (Union Carbide Corporation, Nuclear Division, 1964), by D. W. Burton, Union Carbide Corporation. Nuclear Division, and U.S. Atomic Energy Commission (page images at HathiTrust)
- Equilibrium time for a square plant (United States Atomic Energy Commission, Technical Information Service, 1952), by D. W. Burton, Union Carbide Corporation. Carbide and Carbon Chemicals Company, and U.S. Atomic Energy Commission (page images at HathiTrust)
- Equilibrium time for a square plant (Union Carbide Nuclear Company, Oak Ridge Gaseous Diffusion Plant, 1957), by D. W. Burton, U.S. Atomic Energy Commission, Union Carbide Nuclear Company, and Oak Ridge Gaseous Diffusion Plant (page images at HathiTrust)
- A note on exact and approximate equilibrium time for a square plant (addendum) (Union Carbide Nuclear Company, Oak Ridge Gaseous Diffusion Plant, 1957), by D. W. Burton, U.S. Atomic Energy Commission, Union Carbide Nuclear Company, and Oak Ridge Gaseous Diffusion Plant (page images at HathiTrust)
- The impaction of aerosol particles on cylindrical and spherical collectors (University of Illinois, 1951), by William E. Ranz, University of Illinois at Urbana-Champaign. Engineering Experiment Station, and U.S. Atomic Energy Commission (page images at HathiTrust)
- Particle size distribution in hygroscopic aerosols (Urbana-Champaign, Illinois : University of Illinois, Engineering Experiment Station : 1951., 1953), by G. R. Gillespie, University of Illinois at Urbana-Champaign. Engineering Experiment Station, and U.S. Atomic Energy Commission (page images at HathiTrust)
- Calculating three-dimensional flows around structures and over rough terrain (Los Alamos, New Mexico : Los Alamos Scientific Laboratory of the University of New Mexico, 1971., 1971), by C. W. Hirt, J. L. Cook, Los Alamos Scientific Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
- Theoretical analysis of fluid flow and energy transport in hydrothermal systems (U.S. Dept. of the Interior, Geological Survey, 1977), by Charles R. Faust, James W. Mercer, and Geological Survey (U.S.) (page images at HathiTrust)
- Long range correlations in a closed system with applications to nonuniform fluids (New York, New York : AEC Computing and Applied Mathematics Center, Institute of Mathematical Sciences, New York University, 1960., 1960), by Joel Louis Lebowitz, Jerome K. Percus, U.S. Atomic Energy Commission, and New York University. Institute of Mathematical Sciences (page images at HathiTrust)
- Method for transition prediction in high-speed boundary layers (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Directorate , Wright Laboratory, Air Force Materiel Command, United States Air Force, 1993., 1993), by T. Herbert, Nay Lin, G. K. Stuckert, and Ohio) Wright Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)
Filed under: Aerodynamics -- Mathematical models- User's manual for interactive LINEAR : a FORTRAN program to derive linear aircraft models (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1988), by Robert F. Antoniewicz, Brian P. Patterson, Eugene L. Duke, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Panel methods : an introduction (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Larry L. Erickson and Ames Research Center (page images at HathiTrust)
- Application of supersonic linear theory and hypersonic impact methods to three nonslender hypersonic airplane concepts at mach numbers from 1.10 to 2.86 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by Jimmy L. Pittman, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Sonic-boom wave-front shapes and curvatures associated with maneuvering flight (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by Raymond L. Barger, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Application of a numerically generated orthogonal coordinate system to the solution of inviscid axisymmetric supersonic flow over blunt bodies (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), by H. Harris Hamilton, Randolph A. Graves, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- Development and validation of a combined rotor-fuselage induced flow-field computational method (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), by Carl E. Freeman, Army Research and Technology Laboratories (U.S.). Structures Laboratory, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- Surrogate-equation technique for simulation of steady inviscid flow (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by Gary M. Johnson, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- User's manual for MMLE3, a general FORTRAN program for maximum likelihood parameter estimation (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by Richard E. Maine, Kenneth W. Iliff, Hugh L. Dryden Flight Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Steady subsonic flow around finite-thickness wings (National Aeronautics and Space Administration ;, 1975), by Ching-Chiang Kuo, L. Morino, Langley Research Center, and Boston University. Dept. of Aerospace Engineering (page images at HathiTrust)
- A computer program for wing subsonic aerodynamic performance estimates including attainable thrust and vortex lift effects (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by Harry W. Carlson, Kenneth B. Walkley, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
- Computation of transonic potential flow about three-dimensional inlets, ducts, and bodies (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by Theodore A. Reyhner, Boeing Commercial Airplane Company, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (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)
- A Review of near-wall Reynolds-stress closures (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), by Ronald M. C. So, Langley Research Center, and Arizona State University. College of Engineering and Applied Sciences (page images at HathiTrust)
- Optimum airplane flight paths (National Aeronautics and Space Administration, 1959), by Placido Cicala (page images at HathiTrust)
- Analytical investigation of the motion of a clamshell-type heat shield on deployment from a parent vehicle in the atmosphere (National Aeronautics and Space Administration ;, 1966), by Ross L. Goble and Langley Research Center (page images at HathiTrust)
- 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)
- Electrical characteristics of spark generators for automotive ignition (National Advisory Committee for Aeronautics, 1926), by R. B. Brode, F. B. Silsbee, D. W. Randolph, and Langley Aeronautical Laboratory (page images at HathiTrust)
- Unsteady aerodynamics for advanced configurations. Part IV. Application of the supersonic mach box method to intersecting planar lifting surfaces (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 M. T. Moore, L. V. Andrew, United States. Air Force. Systems Command, Air Force Flight Dynamics Laboratory (U.S.), and North American Aviation. Space and Information Systems Division (page images at HathiTrust)
- Aerodynamic testing in a free-flight spark range (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1997., 1997), by G. L. Winchenbach, Air Force Wright Aeronautical Laboratories, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
- Feedback control for aerodynamics : preprint (Wright Patterson Air Force Base, Ohio : Air Vehicles Directorte, Air Force Research Laboratory, Air Force Materiel Command, 2006., 2006), by R. Chris Camphouse, James H. Myatt, Seddik M. Djouadi, and Ohio). Air Vehicles Directorate Air Force Research Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)
- Unsteady aerodynamics for advanced configurations. Part V. Unsteady potential flow around slender bodies at angles of attack (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 T. C. Li, United States. Air Force. Systems Command, Air Force Flight Dynamics Laboratory (U.S.), and North American Aviation. Space and Information Systems Division (page images at HathiTrust)
- Stability theory for cross hatching. Part I, Linear stability theory (Norton Air Force Base, California : Space and Missile Systems Organization, Air Force Systems Command, United States Air Force, 1972., 1972), by Lester Lees, Denny R. S. Ko, T. Kubota, United States. Air Force. Systems Command, Space and Missile Systems Organization (U.S.), and California Institute of Technology (page images at HathiTrust)
- Unsteady aerodynamics for advanced configurations. Part II A transonic box method for planar lifting surfaces (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 E. R. Rodemich, L. V. Andrew, United States. Air Force. Systems Command, Air Force Flight Dynamics Laboratory (U.S.), and North American Aviation. Space and Information Systems Division (page images at HathiTrust)
- Influence of structural and aerodynamic modeling on flutter analysis and structural optimization (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Directorate, Wright Laboratory, Air Force Systems Command, 1991., 1991), by Alfred G. Struz, Ohio) Wright Laboratory (Wright-Patterson Air Force Base, and University of Oklahoma. School of Aerospace and Mechanical Engineering (page images at HathiTrust)
- The stability of compressible flows and transition through the speed of sound (Wright Field, Dayton, Ohio : Army Air Forces, Air Matériel Command, 1946., 1946), by John Pairman Brown and United States. Army Air Forces. Air Matériel Command (page images at HathiTrust)
- Free-flight range tests of the MK76 MOD 5 Navy practice bobm at Mach numbers of 0.574 to 1.113 (Eglin Air Force Base, Florida : Air Force Armament Laboratory, Guns, Rockets, and Explosives Division, Air Force Systems Command, United States Air Force, 1979., 1979), by G. L. Winchenback, Peter Daniels, Kenneth O. West, United States. Air Force. Systems Command, and Air Force Armament Laboratory (page images at HathiTrust)
- STORESIM : an integrated system for multi-body cfd simulations using unstructured, adaptive grids (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1996., 1996), by M. P. Reddy, Air Force Wright Aeronautical Laboratories, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
- Computational mechanics approach for multidisciplinary nonlinear sensitivity analysis (Arlington, Virginia : Air Force Office of Scientific Research, Air Research and Development Command, United States Air Force, 2001., 2001), by R. V. Grandhi, Wright State University, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
- Unsteady aerodynamics for advanced configurations. Part III. Elliptic-conical wing in linearized unsteady transonic flow (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 E. Albano, L. V. Andrew, United States. Air Force. Systems Command, Air Force Flight Dynamics Laboratory (U.S.), Wright-Patterson Air Force Base. Flight Dynamics Laboratory, and North American Aviation. Space and Information Systems Division (page images at HathiTrust)
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