INDEX 



Taylor, G. I., 30, 39, 50, 205, 210, 212, 



222, 223, 241, 250, 290 

 Taylor turbulence parameter, 31, 57 

 Taylor's cellular ring vortices, 50 

 temperature, 

 defect, 272 



difference ratio, 468, 469 

 distribution, 294, 295, 308 

 effect, 



on bubble growth of, 327 

 on radiation of space variation in, 531 

 mean value in gas radiation, 521 

 of no-fiux walls in enclosure, 529 

 temperature-velocity relationship in tur- 

 bulent boundary layer, 91, 95, 109 

 Tetervin, N., 130, 154 

 Theodorsen, T., 30, 52 

 thermal boundary layer, 437, 442 

 thermal capacity, 278 

 thermal diffusivity, effect on bubble 



growth, 327 

 thermal properties, 

 variable, 280 

 of various materials, 260 

 thermal shield, 

 thick, 277 

 thin, 276 

 thermal shock, 270 

 thermal stresses, 268 

 thermoelastic equations, 269 

 thickness number, hollow cylindrical 



shell, 268 

 three-dimensional effects, 



significance in boundary layers, 156 

 yawed flow, 157 

 Tidstrom, K. D., 15, 45 

 Tollmien, W., 5, 452 

 Tomotika, S., 47 



Townsend, A. A., 144, 159, 164, 166, 168, 

 171, 172, 206, 225, 227, 230, 232, 251 

 transition, 



at boundary of a jet, 52 

 at hypersonic speed, 67 

 at supersonic speed, 54 

 determination by local parameters, 37 

 dimensional analysis, 19 

 effect of, 

 cooling, 397 

 curvature, 8 

 cyUndrical wires, 10, 49 

 distributed roughness, 16 

 flat ridges, 11 

 heat transfer, 53, 54, 63 

 Mach number, 55 

 noise, 46 



nose shape, 54, 57 

 pressure gradient, 6 

 roughness, 8, 38, 49, 62 



transition, effect of, sand-grain rough- 

 ness, 18, 45 



scale of turbulence, 31, 47, 57 



shock waves, 55 



single roughness elements, 8, 61 



spherical roughness elements, 15, 45 



supply turbulence, 399 



surface roughness, 403 



surface temperature, 53 



three-dimensional roughness ele- 

 ments, 15, 45 



turbulence, 30, 41, 47, 55 



two-dimensional roughness elements, 

 10 



waviness, 8, 38, 45 

 in flow between rotating cylinders, 49 

 in pipe, 



of annular cross section, 40 



of circular cross section, 39 



of rectangular cross section, 40 



of square cross section, 40 



with curved axis, 40 



with sharp-edged entrance, 40 

 in propeller wake, 46 

 in rough pipes, 40 

 near rotating disk, 52 

 on airfoUs, 32, 38, 41, 58 



effect of, 



angle of attack, 43 

 roughness, 43 



flight data, 45 

 on airplane configurations, 45 

 on airplanes in flight, 45 

 on bodies of revolution, 46, 47, 49 

 on concave surfaces, 8 

 on cone, 55 

 on cone cylinder, 59 

 on convex surfaces, 8 

 on elliptic cylinder, 41 

 on flat plate, 31, 57 

 on hollow cylinder, 8, 11, 55, 61 

 on ogive cylinder, 59 

 on paraboloid cylinder, 65 

 on prolate spheroid, 48 

 on Rm-10 model, 59, 65 

 on sphere, 46 

 physical mechanism of, 28 

 relation to stability of laminar bound- 

 ary layer, 396 

 transmittance, 



evaluation from gas radiation chart, 534 

 gas, 532 

 transpiration-cooled boundary layer, 

 heat transfer in, 437 

 laminar, 



approximate solution, 438 



compressible, 442 



pressure gradient, 445 



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