B • TURBULENT FLOW 



Kovdsznay, L. S. G. Turbulence in supersonic flow. J. Aeronaut. Sci. 20, 657-675 



(1953). 

 Kovdsznay, L. S. G. Development of turbulence-measuring equipment. NACA 



Rept. 1209, 1954. 

 Laufer, J., and McClellan, R. Measurements of heat transfer from fine wires in 



supersonic flow. /. Fluid Phys. 1, 276-289 (1956). 

 Laurence, J. C., and Landes, L. G. Auxiliary equipment and techniques for adapting 



the constant-temperature hot-wire anemometer to specific problems in air-flow 



measurements. NACA Tech. Note 2843, 1952. 

 Mock, W. C., Jr. Alternating-current equipment for the measurement of fluctuations 



of air speed in turbulent flow. NACA Rept. 598, 1937. 

 Newman, B. G., and Leary, B. G. The measurement of the Reynolds stresses in a 



circular pipe as means of testing a hot wire anemometer. Dept. of Sup-ply, Australia, 



Aeronaut. Research Lab. Rept. A72, 1950. 

 Ossofsky, E. Constant temperature operation of the hot-wire anemometer at high 



frequency. Rev. Sci. Instr. 19, 881-889 (1948). 

 Sansborn, V. A. Heat loss from yawed hot wires at subsonic Mach numbers. NACA 



Tech. Note 3563, 1955. 

 Schubauer, G. B. A turbulence indicator utiUzing the diffusion of heat. NACA Rept. 



524, 1935. 

 Spangenberg, W. G. Heat-loss characteristics of hot-wire anemometers at various 



densities in transonic and supersonic flow. NACA Tech. Note 3381, 1955. 

 Tchen, C. M. Heat delivery in a compressible flow at subsonic and supersonic 



speeds. NACA Tech. Note 2436, 1951. 

 Uberoi, M. S., and Kovasznay, L. S. G. Analysis of turbulent density fluctuations 



by the shadow method. J. Appl. Phys. 26, 1955. 

 Weske, J. R. A hot-wire circuit with very small time lag. NACA Tech. Note 881 1 



1943. 

 Wniis, J. B. Review of hot-wire anemometry. Council for Sci. and Ind. Research, 



Div. of Aeronautics, Australia, Rept. A34, 1945. 

 Wise, B., and Schultz, D. L. Turbulent measurements in supersonic flow with the 



hot-wire anemometer. Brit. Aeronaut. Research Council Rept. FM 2390, 1955. 



B,35. Cited References. 



1. Townsend, A. A. The Structure of Turbulent Shear Flow. Cambridge Univ. 

 Press, 1956. 



2. Batchelor, G. K. The Theory of Homogeneous Turbulence. Cambridge Univ. 

 Press, 1953. 



3. Reynolds, O. Phil. Trans. A186, 123 (1894), or Papers 2, 535. 



4. Lorentz, H. A. Abhandl. theoret. Physik 1, 43 (1907). 



5. Lamb, H. Hydrodynamics, 6th ed. Dover, 1945. 



6. Goldstein, S. Modern Developments in Fluid Dynamics, 1st ed., Vol. 2. Clarendon 

 Press, Oxford, 1938. 



7. Howarth, L. Modern Developments in Fluid Dynamics, High Speed Flow, 

 1st ed., Vol. 2. Clarendon Press, Oxford, 1953. 



8. Rubesin, M. W. A modified Reynolds analogy for the compressible turbulent 

 boundary layer on a flat plate. NACA Tech. Note 2917, 1953. 



9. Crocco, L. Sulla Transmissione del Galore da una Lamina Plana a un Fluido 

 Scorrente ad alta Velocita. Aerotecnica 12, 181-197 (1932). 



10. Squire, H. B. Heat transfer calculation for aerofoils. Brit. Aeronaut. Research 

 Council Repts. and Mem. 1986, 1942. 



11. Ackerman, G. Forsch. Gebiete Ingenieurw. 13, 226-234 (1942). 



12. Mack, L. M. An experimental investigation of the temperature recovery factor. 

 Calif. Inst. Technol. Jet Propul. Lab. Rept. 20-80, 1954. 



13. Stalder, J. R., Rubesin, M. W., and Tendeland, T. A determination of the 

 laminar-transitional, and turbulent-boundary-layer temperature-recovery fac- 

 tors on a flat plate in supersonic flow. NACA Tech. Note 2077, 1950. 



< 190 ) 



