[1] McCroskey WJ, Carr LW, McAlister KW (1976) Dynamic stall experiments on oscillating airfoils. AIAA J 14: 57–63.
[2] McCroskey WJ (1982) Unsteady airfoils. Annual Rev Fluid Mech 14: 285–311.
[3] Chow CY, Chiu CS (1986) Unsteady loading on an airfoil due to vortices released intermittently from its surface. J Aircraft 23: 750–755.
[4] Nakayama A, Stack JP (1993) Surface hot-film technique for measurements of transition, separation, and reattachment points. AIAA 24t h Fluid, Dynamics Conference July 6-9.
[5] Stack P, Mangalam SM, Berry SA (1987) A unique measurement technique to study laminar- separation bubble characteristics on an airfoil. AlAA 87-1271.
[6] Ericsson, Reding LE, JP (1988) Fluid mechanics of dynamic stall. Part I Unsteady flow concept. J Fluids Structures 2: 1–33.
[7] Park SO, Kim JS, Lee, BI (1989) Hot-wire measurements of near wakes behind an oscillating airfoil. AIAA J 28: 22–28.
[8] Chandrasekhara MS, Carr LW (1990) Flow visualization studies of the Mach number effects on dynamic stall of an oscillating airfoil. J Aircraft 27: 516–522.
[9] Lorber PF, Carta Fo (1989) Airfoil stall penetration at constant pitch rate and high Reynolds number. N89-19260.
[10] Lorber PF, Carta Fo (1992) Unsteady transition measurements on a pitching three-Dimensional wing. N93-27450.
[11] Schreck S, Faller, W, Helin H (1994) Pitch rate and Reynolds number effect on unsteady boundary layer transition and separation. AIAA Paper 94-2256.
[12] McCroskey WJ (1997) Computations of unsteady separating flows over an oscillating airfoil. AIAA J 35: 1235–1238.
[13] Moes TR, Sarma GR, Mangalam SM (1997) Flight Demonstration of a Shock Location Sensor Using Constant Voltage Hot- Film Anemometry. NASA Technical Memorandum 4806.
[14] Mangalam AS, Moes TR (2004) Real-Time Unsteady Loads Measurements Using Hot-Film Sensors, AIAA 2004-5371. {Carey, 1998 #8}
[15] Lee T, Basu S (1998) Measurement of unsteady boundary layer developed on oscillating airfoil using multiple hot-film sensors. Exp Fluids 25: 108-117. {Carey, 1998 #8}
[16] Lee T, Gerontakos P, (2004) Investigation of flow over an oscillating airfoil. J Fluid Mech 512: 313–341. {Carey, 1998 #8}
[17] Meijering A, Schroder W (2001) Experimental Analysis of Separated Transitional Transonic Airfoil Flow. AIAA 2001-2987. {Carey, 1998 #8}
[18] Hausmann F, Schroder W (2006) Coated Hot-Film Sensors for Transition Detection in Cruise Flight. J Aircraft 43(2): 456-465. {Carey, 1998 #8}
[19] Kim DH, Chang JW (2010) Unsteady boundary layer for a pitching airfoil at low Reynolds numbers. J Mech Sci Technol 24: 429–440. {Carey, 1998 #8}
[20] Sinclair DW (1996) Measurement techniques applied in a production wind tunnel facility at transonic speeds. AIAA Meeting Papers on Disc. {Carey, 1998 #8}
[21] Amiri, Soltani MR, Haghiri A (2013) Steady flow quality assessment of a modified transonic wind tunnel. Sci Iran B 20 (3): 500–507. {Carey, 1998 #8}
[22] Press WH, Teukolsky SA, Vetterling WT, Flannery BP (2007) Numerical Recipes. The Art of Scientific Computing, Cambridge University Press: 640-642. {Carey, 1998 #8}
[23] Svensdotter S, Fransson T (1998) Hot film and liquid cristal transition measurements in a cscade At varying RE and TU. A98-35273. {Carey, 1998 #8}
[24] Johnson CB, Cmaway DL, Stainback PC, Fancher MF (1987) A Transition Detection Study Using a Cryogenic Hot Film System in the Langley 0.3-Meter Transonic Cryogenic Tunnel. AIAA Paper 87-0049. {Carey, 1998 #8}
[25] Wusk MS, Carraway DL, Holmes BJ (1988) An arrayed hot-film sensor for detection of laminar boundary-layer flow disturbance spatial characteristics. AI AA-88-4677-CP.
[26] Hall RM, Obara CJ, caraway DL, Johnson CB , Azzazy M (1989) Comparisons of boundary-layer transition measurement techniques in the langley unitary plan wind tunnel. AIAA 89-2205-CP. {Carey, 1998 #8}
[27] Ida F, Kunikyo T, Nakasu K, Shinohara J, Experimental Quantitative Turbine Boundary-Layer Investigations Using Multiple Hot Film Sensor, AIAA 94-2537. {Carey, 1998 #8}
[28] Ubaldi M, Zunino P (2006) Boundary layer transition on the suction side of a turbine blade. Proceedings of the 2nd WSEAS Int. Conference on Applied and Theoretical Mechanics, Venice, Italy.{Carey, 1998 #8}
[29] Olivani A, Halter F, Yoshida A, Gökalp I (2005) Experimental characterization of turbulence spectra and scales in high pressure turbulent premixed flames. Proceedings of the European Combustion Meeting.{Carey, 1998 #8}
[30] Canepa E, Ubaldi M, Zunino P (2002) Experiences in the application of intermittency detection techniques to hot film signals in transitional boundary layers. The 16th Symposium on Measuring Techniques in Transonic and Supersonic Flow in Cascades and Turbomachines. {Carey, 1998 #8}
[31] Schlichting H, Kestin J (Translator) (2000) Boudary-layer theory. 7th edn. McGraw-Hill, New York
)