Książki na temat „Aircraft wake”

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1

Hallock, J. N. Aircraft wake vortices: An annotated bibliography (1923-1990). Washington D.C: Research and Development Service, U.S. Dept. of Transportation, Federal Aviation Administration, 1991.

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2

C, Miake-Lye R., i Langley Research Center, red. Stratospheric aircraft exhaust plume and wake chemistry studies. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

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3

E, Marshall Robert. Radar reflectivity in wingtip-generated wake vortices. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

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4

Blackmore, Paul. Slate and tile roofs: Avoiding damage from aircraft wake vortices. Watford: CRC, 2002.

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5

Center, Langley Research, red. Feasibility of detecting aircraft wake vortices using passive microwave radiometers. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

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6

Center, Langley Research, red. Characterizing the wake vortex signature for an active line of sight remote sensor. Clemson, SC: Radar Systems Laboratory, Electrical and Computer Engineering Dept., Clemson University, 1994.

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7

Severin, Theresa Ann. In the wake of the storm: Living beyond the tragedy of Flight 4184. Arlington Heights, IL: North Cross Press, 2008.

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8

Bilanin, Alan J. Interaction of spray aircraft wake with convective surface winds in hilly terrain. Davis, CA: USDA Forest Service, 1996.

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9

Vyshinski, V. V. Flight safety, aircraft vortex wake and airport operation capacity: Collection of papers. Moscow: [s.n.], 2002.

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10

Clark, Richard A. Back to the Bennington: Tales in the wake. Bennington, VT: Merriam Press, 2010.

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11

D, Campbell S., i Langley Research Center, red. Wake vortex field measurement program at Memphis, Tennessee: Data guide. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

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12

Hinton, David A. A candidate wake vortex strength definition for application to the NASA Aircraft Vortex Spacing System (AVOSS). Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

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13

Liu, Chen Huei. Navier-Stokes calculations for the vortex wake of a rotor in hover. New York: American Institute of Aeronautics and Astronautics, 1993.

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14

C, Zheng Z., i Institute for Computer Applications in Science and Engineering., red. 3D visualization of unsteady 2D airplane wake vortices. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1994.

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15

United States. National Aeronautics and Space Administration., red. Prediction and control of vortex-dominated and vortex-wake flows. Norfolk, Va: Old Dominion University Research Foundation, 1993.

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16

Block, P. J. W. Directory and trends of noise generated by a propeller in a wake. Hampton, Va: Langley Research Center, 1986.

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17

Norman, Tom. Application of the wide-field shadowgraph technique to rotor wake visualization. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.

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18

Norman, Tom. Application of the wide-field shadowgraph technique to rotor wake visualization. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.

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19

Norman, Tom. Application of the wide-field shadowgraph technique to rotor wake visualization. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.

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20

Mackenzie, Anne I. Measured changes in C-band radar reflectivity of clear air caused by aircraft wake vortices. Washington, D.C: National Aeronautics and Space Administration, 1997.

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21

Center, Langley Research, red. Measured changes in C-band radar reflectivity of clear air caused by aircraft wake vortices. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

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22

Center, Langley Research, red. Measured changes in C-band radar reflectivity of clear air caused by aircraft wake vortices. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

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23

Dynamics, Inc Continuum. Field study of interaction of spray aircraft wake with convective surface winds in hilly terrain. Davis, CA: United States Department of Agriculture, Forest Service, Forest Health Protection, Forest Health Technology Enterprise Team, 1996.

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24

Center, Langley Research, red. Measured changes in C-band radar reflectivity of clear air caused by aircraft wake vortices. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

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25

Center, Langley Research, red. Measured changes in C-band radar reflectivity of clear air caused by aircraft wake vortices. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

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26

Mackenzie, Anne I. Measured changes in C-band radar reflectivity of clear air caused by aircraft wake vortices. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

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27

L, Clawson K., i Air Resources Laboratory (U.S.), red. Vortex wake characteristics of B757-200 and B767-200 aircraft using the tower fly-by technique. Silver Spring, Md: U.S. Dept. of Commerce, National Oceanic and Atmospheric Administration, Environmental Research Laboratories, Air Resources Laboratory, 1993.

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28

Center, Langley Research, red. A parametric study of accelerations of an airplane due to a wake vortex system. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

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29

C, Stewart Eric, Rivers Robert A i United States. National Aeronautics and Space Administration., red. Overview of the preparation and use of an OV-10 aircraft for wake vortex hazards flight experiments. Washington, D.C: AIAA, 1995.

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30

C, Zheng Z., Old Dominion University. Research Foundation. i United States. National Aeronautics and Space Administration., red. Initialization and simulation of three-dimensional aircraft wake vortices: Final report for the period ending May 1997, under grant# NAG-1-1437. Norfolk, Va: Dept. of Aerospace Engineering, College of Engineering and Technology, Old Dominion University, 1997.

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31

Tatnall, Christopher Rhoads. An investigation of candidate sensor-observable wake vortex strength parameters for the NASA Aircraft Vortex Spacing System (AVOSS). Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

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32

United States. National Aeronautics and Space Administration., red. Prediction and control of vortex-dominated and vortex-wake flows: Final report for the period December 1, 1993 through December 1, 1995. Norfolk, Va: Old Dominion University Research Foundation, 1996.

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33

Doggett, Robert V. Flutter clearance flight tests of an OV-10A airplane modified for wake vortex flight experiments. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

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34

Doggett, Robert V. Flutter clearance flight tests of an OV-10A airplane modified for wake vortex flight experiments. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

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35

Lin, Yuh-Lang. Numerical modeling studies of wake vortex transport and evolution within the planetary boundary layer: FY94 July semi-annual report. Raleigh, NC: Dept. of Marine, Earth and Atmospheric Sciences, North Carolina State University, 1994.

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36

Pal, Arya S., Kaplan Michael L i United States. National Aeronautics and Space Administration., red. Numerical modeling studies of wake vortex transport and evolution within the planetary boundary layer: FY94 July semi-annual report. Raleigh, NC: Dept. of Marine, Earth and Atmospheric Sciences, North Carolina State University, 1994.

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37

United States. Congress. House. Committee on Science, Space, and Technology. Subcommittee on Technology, Environment, and Aviation. Application of FAA wake vortex research to safety: Hearing before the Subcommittee on Technology, Environment, and Aviation of the Committee on Science, Space, and Technology, U.S. House of Representatives, One Hundred Third Congress, second session, July 28, 1994. Washington: U.S. G.P.O., 1995.

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38

Ginevsky, A. S., i A. I. Zhelannikov. Vortex wakes of Aircrafts. Berlin, Heidelberg: Springer Berlin Heidelberg, 2009. http://dx.doi.org/10.1007/978-3-642-01760-5.

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39

Williamson, Guy G. Experimental study of aircraft wakes in forest canopies. Missoula, MT: The Center, 1986.

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40

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., red. Aircraft propeller induced structure-borne noise. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

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41

Harvey, J. K. Dispersion in the wakes of aircraft: An investigation of the effects of a ground plane on trailing vortices. London: Imperial College of Science and Technology, 1986.

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42

Center, Langley Research, red. Stereo-video data reduction of wake vortices and trailing aircrafts. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

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43

Alter-Gartenberg, Rachel. Stereo-video data reduction of wake vortices and trailing aircrafts. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

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44

Zaloga, Steve. Russian Falcons: The new wave of Russian combat aircraft. Hong Kong: Concord Publications Co., 1992.

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45

Gray, Robert D. Systematic wage administration in the southern California aircraft industry. New York: Industrial Relations Counselors, 1988.

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46

Zaloga, Steve. Russian Falcons: The new wave of Russian combat aircraft. Hong Kong: Concord Publications Co., 1992.

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47

K, Rutishauser David, i Langley Research Center, red. Enhanced airport capacity through safe, dynamic reductions in aircraft separation: NASA's Aircraft Vortex Spacing System (AVOSS). Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2001.

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48

Soderman, Paul T. Acoustic and aerodynamic study of a pusher-propeller aircraft model. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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49

W, Hicks John, i United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., red. In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisions with contemporary aircraft). [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1994.

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50

W, Hicks John, i United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., red. In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisions with contemporary aircraft). [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1994.

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