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Books on the topic 'Over-flow'

Author: Grafiati

Published: 3 June 2025

Last updated: 31 July 2025

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1

Thompson, LuAnne. Flow over finite isolated topography. Woods Hole Oceanographic Institution, 1990.

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2

Rennick, Mary Alice. Air flow over large scale topography. Naval Postgraduate School, 1989.

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3

Pidd, M. Asymmetric vortex flow over circular cones. HMSO, 1991.

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4

Blom, P. Turbulent free-surface flow over a sill. Faculty of Civil Engineering, Delft University of Technology, 1993.

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5

Bernhard, Müller, and Rues D. 1930-, eds. 3D viscous hypersonic flow over blunt bodies. DFVLR, 1989.

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6

Uwe, Dallmann, and Deutsche Forschungs- und Versuchsanstalt für Luft- und Raumfahrt., eds. Flow over a leading edge with distributed roughness. DFVLR, 1988.

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7

Srivastava, Rakesh. Simulation of unsteady rotational flow over propfan configuration. National Aeronautics and Space Administration, 1990.

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8

Jiunn-Chi, Wu, Sankar Lakshmi N, and United States. National Aeronautics and Space Administration., eds. Analysis of viscous transonic flow over airfoil sections. National Aeronautics and Space Administration, 1987.

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9

Jiunn-Chi, Wu, Sankar L. N, and United States. National Aeronautics and Space Administration., eds. Analysis of viscous transonic flow over airfoil sections. National Aeronautics and Space Administration, 1987.

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10

Srivastava, Rakesh. Simulation of unsteady rotational flow over propfan configuration. National Aeronautics and Space Administration, 1990.

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11

Ravindran, S. S. Active control of flow separation over an airfoil. National Aeronautics and Space Administration, Langley Research Center, 1999.

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12

Ravindran, S. S. Active control of flow separation over an airfoil. National Aeronautics and Space Administration, Langley Research Center, 1999.

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13

Philip, Hall, and Institute for Computer Applications in Science and Engineering., eds. The stability of two-phase flow over a swept-wing. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1994.

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14

Philip, Hall, and Institute for Computer Applications in Science and Engineering., eds. The stability of two-phase flow over a swept-wing. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1994.

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15

Philip, Hall, and Institute for Computer Applications in Science and Engineering., eds. The stability of two-phase flow over a swept-wing. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1994.

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16

Ghorbanian, K. Supersonic flow of reactive gases over sphere-cone bodies. American Institute of Aeronautics and Astronautics, 1992.

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17

Kjelgaard, Scott O. Detailed flow-field measurements over a 75⁰ swept delta wing. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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18

Kjelgaard, Scott O. Detailed flow-field measurements over a 75⁰ swept delta wing. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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19

Ruprecht, Albert. Prediction of turbulent flow over a backward-facing step. Imperial College of Science and Technology, 1986.

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20

Center, Langley Research, ed. Hypersonic, nonequilibrium flow over a cylindrically blunted 6 wedge. National Aeronautics and Space Administration, Langley Research Center, 1993.

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21

Miller, D. S. Lee-side flow over delta wings at supersonic speeds. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

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22

Gnoffo, Peter A. Hypersonic, nonequilibrium flow over a cylindrically blunted 6ʻ́ wedge. National Aeronautics and Space Administration, Langley Research Center, 1993.

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23

M, Wood Richard, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Lee-side flow over delta wings at supersonic speeds. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

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24

M, Wood Richard, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Lee-side flow over delta wings at supersonic speeds. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

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25

Gudmundsson, G. Hilmar. Glacier sliding over sinusoidal bed and the characteristics of creeping flow over bedrock undulations. Versuchsanstalt für Wasserbau, Hydrologie und Glaziologie, Eidgenössische Technische Hochschule Zürich, 1994.

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26

Leighton, T. G. Sonoluminescence from flow over a hydrofoil in a cavitation tunnel. University of Southampton, Institute of Sound and Vibration Research, 1993.

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27

Venkit, Iyer, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Transition prediction and control in subsonic flow over a hump. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

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28

Venkit, Iyer, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Transition prediction and control in subsonic flow over a hump. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

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29

Sajjadi, S. G. Second-moment closure modelling of turbulent flow over sand ripples. University of Salford Centre for Computational Fluid Dynamics and Turbulence, 1993.

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30

Boyer, D. L. Linearly stratified, rotating flow over long ridges in a channel. RoyalSociety, 1986.

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31

K, Hebbar Sheshagiri, and Ames Research Center, eds. Three-dimensional turbulent boundary layer flow over a spinning cylinder. National Aeronautics and Space Administration, Ames Research Center, 1991.

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32

Driver, David M. Three-dimensional turbulent boundary layer flow over a spinning cylinder. National Aeronautics and Space Administration, Ames Research Center, 1991.

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33

Yousuff, Hussaini M., and Institute for Computer Applications in Science and Engineering, eds. Incipient transition phenomena in compressible flow over a flat plate. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1986.

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34

Yousuff, Hussaini M., and Institute for Computer Applications in Science and Engineering., eds. Incipient transition phenomena in compressible flow over a flat plate. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1986.

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35

Driver, David M. Three-dimensional turbulent boundary layer flow over a spinning cylinder. National Aeronautics and Space Administration, Ames Research Center, 1991.

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36

Driver, David M. Three-dimensional turbulent boundary layer flow over a spinning cylinder. National Aeronautics and Space Administration, Ames Research Center, 1991.

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37

Kjelgaard, Scott O. Detailed flow-field measurements over a 75 degree swept delta wing. Langley Research Center, 1990.

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38

Flowe, Ken. Over Flow on Clear Creek: Descendants of James Flow (1821-1877) and David Flough (ca. 1740-1792). Gateway Press, 2004.

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39

Muller, Bernhard. Navier-Stokes solutions for laminar transonic flow over a NACA0012 airfoil. The Aeronautical Research Institute of Sweden, 1986.

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40

Chaussee, D. S. Numerical simulation of viscous supersonic flow over a generic fighter configuration. National Aeronautics and Space Administration, Ames Research Center, 1986.

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41

Chaussee, D. S. Numerical simulation of viscous supersonic flow over a generic fighter configuration. National Aeronautics and Space Administration, Ames Research Center, 1986.

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42

Kozel, Karel. Numerical simulation of two-dimensional transonic flow over thin oscillating airfoil. Information Centre for Aeronautics, 1986.

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43

Chambers, Lin Hartung. Hypersonic, nonequilibrium flow over the FIRE II forebody at 1634 sec. National Aeronautics and Space Administration, Langley Research Center, 1994.

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44

Miura, H. Oblique shock waves in a dusty-gas flow over a wedge. [s.n.], 1986.

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45

E, Melnik R., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, eds. GRUMFOIL, a computer code for the viscous transonic flow over airfoils. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

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46

Thompson, D. H. Visualisation in water of vortex flow over sharp-edged canard configurations. Australia, Dept. of Defence, Aeronautical Research Laboratory, 1992.

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47

Nelson, John. Boundary layer flow of air over water on a flat plate. National Aeronautics and Space Administration, Langley Research Center, 1993.

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48

Griffiths, Stephen. Simulation of separated flow over aerofoils at high angles of incidence. UMIST, 1997.

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49

E, Melnik R., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. An improved viscid/inviscid interaction procedure for transonic flow over airfoils. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

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50

Roberts, Thomas W. Euler equation computations for the flow over a hovering helicopter rotor. National Aeronautics and Space Administration, 1988.

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