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1

Jet Propulsion Laboratory (U.S.) and Solar Energy Research Institute, eds. Flat-plate Solar Array Project. Pasadena, Calif: Jet Propulsion Laboratory, 1988.

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2

Perers, Bengt. Flat plate collectors with booster mirrors. Stockholm: Swedish Council for Building Research, 1993.

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3

Maddocks, M. C. D. A flat-plate antenna for DBS reception. London: BBC, 1988.

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4

D, Mehta R., and Ames Research Center, eds. Asymptotic behavior of a flat plate wake. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.

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5

Dogra, Virendra K. Rarefied flow past a flat plate at incidence. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.

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6

Maddocks, M. C. D. Polarisation converters for a DBS flat-plate antenna. London: BBC, 1988.

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7

Andreas, Acrivos, and United States. National Aeronautics and Space Administration., eds. Forced convection and sedimentation past a flat plate. [Washington, DC: National Aeronautics and Space Administration, 1995.

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8

Maddocks, M. C. D. Array elements for a DBS flat-plate antenna. London: BBC, 1988.

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9

Allan, Brian G. Simulation of embedded streamwise vortices on a flat plate. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 2002.

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10

Marion, William. Solar radiation data manual for flat-plate and concentrating collectors. Golden, Colo: National Renewable Energy Laboratory, 1994.

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11

Pao, Yih-Ho. Time-dependent viscous incompressible flow past a finite flat plate. [Seattle, Wash.]: Boeing Scientific Research Laboratories, Flight Sciences Laboratory, 1986.

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12

Pao, Yih-Ho. Time-dependent viscous incompressible flow past a finite flat plate. [Seattle, Wash.]: Boeing Scientific Research Laboratories, Flight Sciences Laboratory, 1986.

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13

Stephen, Cowley, Hall Philip, and Langley Research Center, eds. On the instability of hypersonic flow past a flat plate. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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14

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

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15

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

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16

Erlebacher, Gordon. Incipient transition phenomena in compressible flows over a flat plate. Hampton, Va: ICASE, 1986.

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17

Heinrich, Roland Adolf Eberhard. Flat plate leading edge receptivity to various freestream disturbance structures. [Tucson, Ariz.]: University of Arizona, 1989.

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18

Blackaby, Nicholas D. On the instability of hypersonic flow past a flat plate. Hampton, Va: Institute for Computer Applications in Science and Engineering, 1990.

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19

Wakeling, S. Beamforming devices and feed structures for a DBS flat-plate antenna. London: BBC, 1989.

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20

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

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21

Wilmoth, Richard G. Interference effects on the hypersonic, rarefied flow about a flat plate. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.

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22

Colloquium on flat plate and low profile mobile antennas (1990 London). Flat plate and low profile mobile antennas, Savoy Place [London] on Wednesday 10 January 1990. London: Institution of Electrical Engineers, 1990.

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23

Kogan, M. N. Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate). Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

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24

Chow, L. C. Safety review package for University of Central Florida flat-plate heat pipe experiment. [Washington, DC: National Aeronautics and Space Administration, 1998.

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25

A, Wardwell Douglas, and Ames Research Center, eds. Jet-induced ground effects on a parametric flat-plate model in hover. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1993.

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26

A, Wardwell Douglas, and Ames Research Center, eds. Jet-induced ground effects on a parametric flat-plate model in hover. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1993.

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27

Patrick, William P. Flowfield measurements in a separated and reattached flat plate turbulent boundary layer. Cleveland, Ohio: Lewis Research Center, 1987.

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28

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. Flowfield measurements in a separated and reattached flat plate turbulent boundary layer. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

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29

A, Wardwell Douglas, and Ames Research Center, eds. Jet-induced ground effects on a parametric flat-plate model in hover. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1993.

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30

A, Wardwell Douglas, and Ames Research Center, eds. Jet-induced ground effects on a parametric flat-plate model in hover. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1993.

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31

Maestrello, Lucio. Relaminarization of turbulent flow on a flat plate by localized surface heating. Washington, D. C: AIAA, 1989.

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32

M, Llorente Ignacio, Salas M. D, and Institute for Computer Applications in Science and Engineering., eds. Semicoarsening and implicit smoothers for the simulation of a flat plate at yaw. Hampton, VA: ICASE, NASA Langley Research Center, 2001.

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33

N, Kogan M., and Langley Research Center, eds. Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate): Final report. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

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34

Allen, Jerry M. Parametric fin-body and fin-plate database for a series of 12 missile fins. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2001.

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35

Allen, Jerry M. Parametric fin-body and fin-plate database for a series of 12 missile fins. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2001.

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36

Allen, Jerry M. Parametric fin-body and fin-plate database for a series of 12 missile fins. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2001.

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37

Center, Langley Research, ed. Parametric fin-body and fin-plate database for a series of 12 missile fins. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2001.

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38

Terry, Ng T., Nelson Robert C. 1942-, United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., University of Notre Dame. Dept. of Aerospace and Mechanical Engineering., and Ames Research Center, eds. Visualization of leading edge vortices on a series of flat plate delta wings. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.

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39

Yu, Ping, Scott John Dip Ed, and United States. National Aeronautics and Space Administration., eds. Time domain numerical calculations of unsteady vortical flows about a flat plate airfoil. [Washington, DC]: National Aeronautics and Space Administration, 1989.

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40

United States. National Aeronautics and Space Administration., ed. Design of high-Reynolds-number flat-plate experiments in the NTF: Final report. Tempe, Ariz: Dept. of Mechanical and Aerospace Engineering, Arizona State University, 1989.

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41

United States. National Aeronautics and Space Administration., ed. Design of high-Reynolds-number flat-plate experiments in the NTF: Final report. Tempe, Ariz: Dept. of Mechanical and Aerospace Engineering, Arizona State University, 1989.

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42

Maestrello, Lucio. Numerical study of three-dimensional spatial instability of a supersonic flat plate boundary layer. Hampton, Va: ICASE, 1989.

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43

Alvin, Bayliss, Krishnan Ramachander, and Langley Research Center, eds. Numerical study of three-dimensional spatial instability of a supersonic flat plate boundary layer. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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44

United States. National Aeronautics and Space Administration., ed. Friction factor data for flat plate tests of smooth and honeycomb surfaces: A thesis. [College Park, Tex.?]: Texas A&M University, Turbomachinery Laboratory, Mechanical Engineering Dept., 1989.

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45

Conley, Julianne M., and Patrick L. Zeman. Verification of the proteus two-dimensional Navier-Stokes code for flat plate and pipe. [Washington, D.C.]: National Aeronautics and Space Administration, 1991.

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46

Flamm, Jeffrey D. Drag measurements of an axisymmetric nacelle mounted on a flat plate at supersonic speeds. [Hampton, Va.]: National Aeronautics and Space Administration, Langley Research Center, 1995.

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47

Wilcox, Floyd J. Drag measurements of blunt stores tangentially mounted on a flat plate at supersonic speeds. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

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48

Kogan, M. N. Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate): Under cooperative agreement NCC1-241. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

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49

Kogan, M. N. Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate): Under cooperative agreement NCC1-241. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

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50

Kogan, M. N. Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate): Under cooperative agreement NCC1-241. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

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