1Spina E F,Mcginley C B.Constant-temperature anemometryin hypersonic flow:critical issues and sample results[J].Experimentsin Fluids,1994,17(6):365-374.
2King L V.Onthe convection of heatfromsmall cylindersin a streamof fluid:Determination of the convection constants of small plati-numwires with applications to hot-wire anemometry[J].Phil.Trans.Roy.Soc,1914:373-432.
3Kovasznay,Leslie S G.The hot-wire anemometer in supersonic flow[J].Journal of the Aeronautical Sciences,1950,17(9):565-573.
4Lowell HH.Design and applications of hot-wire anemometerfor steady-state measurements at transonic and supersonic airspeed[R].NASATN-2117,1950.
5Acharya M.Measurements of turbulent fluctucationin high-speedflows using hot-wires and hot-films[J].Reviewof Scientific Instru-ments,1979,50(8):952-957.
6Bestion D.Comparison between constant-current and constat-temperature hot-wire anemometersin highspeedflows[J].Rev.Sci.In-strum,1983,54(11):1514-1524.
7Logan P.Modal analysis of hot-wire measurements in supersonic turbulence[R].AIAA-88-0423,1988.
8Comte-Bellot G,Sarma G R,Faure T M.Performance studies of the constant voltage anemometer in a mach 2.3 boundary layer[C].18thInternational Congress onInstrumentationin Aerospace Simulation Facilities,Toulouse,France,June,1999:40/1-40/9.
9Lecic MR.Anewexperimental approachtothe calibration of hot-wire probes[J].Flow Measurement and Instrumentation,2009,20(3):136-140.
10John E L.Observations of hypersonic boundary-layer transition[J].AIAAJournal,1972,10(6):762-769.
