Books on the topic 'Reynolds Range'

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1

Pfenninger, Werner. Optimization of natural laminar flow airfoils for high section lift-to-drag ratios in the lower Reynolds number range. Washington, D. C: AIAA, 1989.

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2

Parsons, Chuck. Texas Ranger N.O. Reynolds, the intrepid. Honolulu, HI: Talei Publishers, 2005.

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3

author, Brice Donaly E., ed. Texas Ranger N.O. Reynolds, the Intrepid. Denton, Texas: University of North Texas Press, 2014.

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4

J, Boyle R., and Lewis Research Center, eds. Aerodynamics of a transitioning turbine stator over a range of Reynolds numbers. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

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5

D, Moore Royce, United States. Army Aviation Research and Technology Activity., and United States. National Aeronautics and Space Administration., eds. Performance of two 10-lb/sec centrifugal compressors with different blade and shroud thicknesses operating over a range of Reynolds numbers. [Washington, DC]: National Aeronautics and Space Administration, 1987.

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6

D, Moore Royce, United States. Army Aviation Research and Technology Activity., and United States. National Aeronautics and Space Administration., eds. Performance of two 10-lb/sec centrifugal compressors with different blade and shroud thicknesses operating over a range of Reynolds numbers. [Washington, DC]: National Aeronautics and Space Administration, 1987.

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7

Performance of two 10-lb/sec centrifugal compressors with different blade and shroud thicknesses operating over a range of Reynolds numbers. [Washington, DC]: National Aeronautics and Space Administration, 1987.

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8

R, Whetstone James, and National Institute of Standards and Technology (U.S.), eds. Measurements of coefficients of discharge for concentric flange-tapped square-edged orifice meters in water over the Reynolds number range 600 to 2,700,000. Gaithersburg, MD: U.S. Dept. of Commerce, National Institute of Standards and Technology, 1989.

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9

Measurements of coefficients of discharge for concentric flange-tapped square-edged orifice meters in natural gas over the Reynolds number range 25,000 to 16,000,000. Gaithersburg, MD: U.S. Dept. of Commerce, National Institute of Standards and Technology, 1989.

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10

Biewener, Andrew A., and Shelia N. Patek, eds. Movement in Water. Oxford University Press, 2018. http://dx.doi.org/10.1093/oso/9780198743156.003.0005.

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This chapter examines how the physical properties of water influence and explain the great diversity of swimming performance and mechanisms - from the scale of spermatozoa on up to whales. The key parameters of inertia, viscosity and their manifestation in the critically important Reynolds number are explained and placed in the context of a range of swimming mechanisms, including undulatory movement and fin-based, jet-based, flagellar and ciliary propulsion. The air-water interface also presents an intriguing mechanical challenge for the many organisms that move on top of the water’s surface. The chapter concludes with a brief overview of the burgeoning field of biorobotic swimmers.
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11

Nolon, Sean. Arbitration and the Olympic Athlete. Edited by Michael A. McCann. Oxford University Press, 2017. http://dx.doi.org/10.1093/oxfordhb/9780190465957.013.25.

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Disputes involving Olympic athletes can arise from a wide range of decisions made by a host of entities. A disputed decision may involve the eligibility of an athlete, employment of coaches and staff, organizational governance, doping, and commercial contracts. Three disputes involving athletes and the modern Olympic games show how arbitration has come to play a central role in resolving contested decisions of sporting associations. First, the case of sprinter Harry Reynolds illustrates the limitations of using national courts to challenge doping-related sanctions. Second, the eligibility struggles of Oscar Pistorius demonstrate how athletes and national sporting associations can benefit from arbitration’s efficiency. Finally, the case of Claudia Pechstein offers a recent example showing the deference given arbitration by national courts, for better or worse.
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12

Escudier, Marcel. Turbulent flow. Oxford University Press, 2018. http://dx.doi.org/10.1093/oso/9780198719878.003.0018.

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In this chapter the principal characteristics of a turbulent flow are outlined and the way that Reynolds’ time-averaging procedure, applied to the Navier-Stokes equations, leads to a set of equations (RANS) similar to those governing laminar flow but including additional terms which arise from correlations between fluctuating velocity components and velocity-pressure correlations. The complex nature of turbulent motion has led to an empirical methodology based upon the RANS and turbulence-transport equations in which the correlations are modelled. An important aspect of turbulent flows is the wide range of scales involved. It is also shown that treating near-wall turbulent shear flow as a Couette flow leads to the Law of the Wall and the log law. The effect of surface roughness on both the velocity distribution and surface shear stress is discussed. It is shown that the distribution of mean velocity within a turbulent boundary layer can be represented by a linear combination of the near-wall log law and an outer-layer Law of the Wake.
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13

Experimental surface pressure data obtained on 65 ̊delta wing across Reynolds number and Mach number ranges. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

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14

Reynolds, Frederick. The Rage: A Comedy. As it is Performed at the Theatre-Royal, Covent-Garden. By Frederick Reynolds. The Third Edition. Gale ECCO, Print Editions, 2018.

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15

United States. National Aeronautics and Space Administration., ed. EXPERIMENTAL SURFACE PRESSURE DATA OBTAINED ON 65 DEG DELTA WING ACROSS REYNOLDS NUMBER AND MACH NUMBER RANGES... NASA-TM-4645-VOL-2 ... MAR. [S.l: s.n., 1998.

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