Eksperymentalne badania wpływu wirów wzdłużnych na niestacjonarne oderwanie

• Autorzy: Telega Janusz
• Języki publikacji: PL

Słowa kluczowe

PL

lotnictwo; wiry wzdłużne; generatory wirów; fale uderzeniowe

• Wydawca: Wydawnictwo Instytutu Maszyn Przepływowych PAN
• Czasopismo: Zeszyty Naukowe Instytutu Maszyn Przepływowych Polskiej Akademii Nauk w Gdańsku
• Rocznik: 2019
• Tom: nr 565/1524
• Strony: 3--282
• Opis fizyczny: Bibliogr. 27 poz., rys., tab.

Twórcy

autor

Telega Janusz

• Instytut Maszyn Przepływowych PAN

Bibliografia

• [1] R. A. Wallis. The use of air jets for boundary layer control. A.R.L. Aeronote, 1952.
• [2] R. A. Wallis. A preliminary note on a modified type of air jet for boundary layer control. Aeronautical Research Council-A.R.C. C.P.513, 1956.
• [3] R. A. Wallis, Sturat C. M. On the control of shock-induced boundarylayer separation with discrete air jets. Aeronautical Research CouncilA.R.C., Rep. 19865, 1956.
• [4] C. M. Velte, M. O. L. Hansen, D. Cavar. Flow analysis of vortex generators on wing sections by stereoscopic particle image velocimetry measurements. Enviromental Research Letters, 2008.
• [5] H. Pearcy. Shock induced separation and its prevention by design and boundary layer control. Pergamon Press, Vol.2, strony 1166–1344, 1961.
• [6] N. C. Freeman, R. F. Cash. Experiments with slot blowing and discrete air jets to suppress shock-induced separation. Unpublished N.P.L. (National Phisical Laboratory) work, 1958.
• [7] A. B. Haines, T. E. Bateman. Report draft. Unpublished N.P.L. (National Phisical Laboratory) work, 1959.
• [8] J. P. Johnston, M. Nishi. Vortex generator jets – a means for flow separation control. AIAA Journal, Vol. 28, No.6, strony 989–994, 1990.
• [9] D. A. Compton, J. P. Johnston. Streamwise vortex production by pitched and skewed jets in a turbulent boundary layer layer. AIAA Journal, Vol. 30, No. 3, strony 640–647, 1992.
• [10] Z. U. Khan, J. P. Johnston. On vortex generating jets. International Journal of Heat and Fluid Flow 21, strony 506–511, 2000.
• [11] Z. U. Khan, J. P. Johnston. On the dominant vortex produced by a pitched and skewed jet in crossflow. Thermoscience Division, Mechanical Engineering Department, Stanford University, 1999.
• [12] J. P. Johnston, B. P. Mosier, Z. U. Khan. Vortex generating jets; effects of jet-hole inlet geometry. International Journal of Heat and Fluid Flow, strony 744–749, 2002.
• [13] G. V. Selby, J. C. Lin, F.G. Howard. Control of low-speed turbulent separated flow using jet vortex generators. Experiments in Fluids 12, strony 394–400, 1992.
• [14] M. K. Rao. An experimental investigation of the use of air-jet vortex generators to control shock-induced boundary layer separation. PhD Thesis, City University, London, 1988.
• [15] H. H. Pearcey, M. K. Rao, D. M. Sykes. Inclined air-jets used as vortex generators to suppress shock-induced separation. AGARD Meeting on Computational and Experimental Assessment of Jets in Cross Flow, 1993.
• [16] X. Zhang, M. W. Collins. Nearfield evaluation of a longitudinal vortex generated by an inclined jet in a turbulent boundary layer. ASME Journal of Fluids Engineering, Vol. 119, strony 934–939, 1997.
• [17] X. Zhang. Turbulence measurements of longitudinal vortex generated by an inclined jet in a turbulent boundary layer. ASME Journal of Fluids Engineering, Vol.120, strony 765–771, 1998.
• [18] X. Zhang. An inclined rectangular jet in a turbulent boundary layervortex flow. Experiments in Fluids, Vol. 28, strony 344–354, 2000.
• [19] X. Zhang. Turbulence measurements of an inclined rectangular jet in a turbulent boundary layer. International Journal of Heat and Fluid Flow, strony 292–296, 2000.
• [20] I. M. Milanowic, K. B. Zaman. Pitched and yawed circular jest in cross-flow. ASME Fluids Egineering Division Summer Meeting, strony 292–296, 2002.
• [21] L. J. Souverein, J. F. Debieve. Effect of air-jet vortex generators on a shock wave boundary layer interaction. Exp. Fluids 49, strony 1053– 1064, 2010.
• [22] W. J. Prosnak. Mechanika Płynów, Tom I i II. Wydawnictwo Naukowe PWN, wydanie 1, 1970.
• [23] S. Discetti, A. Ianiro. Experimental Aerodynamics. CRC Press, Taylor & Francis Group, wydanie 1, 2017.
• [24] A.F.P. Houwing, K.Takayama, Z.Jiang, M.Sun, K.Yada, H.Mitobe. Interferometric measurement of density in nonstationary shock wave reflection flow and comparison with cfd. Shock Waves, 2005.
• [25] D.J. Bone. Fourier fringe analysis-the two-dimensional phase unwrapping problem. Applied Optics, 1991.
• [26] H. Liepmann, W. Roshko. Elements of Gas Dynamics. John Wiley and Sons, New York, 1957.
• [27] R. Szwaba, K. Namieśnik. Design of a nozzle for the flow control for ufast wp-3 project. Opracowanie wewnętrzne Instytutu Maszyn Przepływowych PAN, nr arch. 5146/05, 2005.

Uwagi

Opracowanie rekordu ze środków MNiSW, umowa Nr 461252 w ramach programu "Społeczna odpowiedzialność nauki" - moduł: Popularyzacja nauki i promocja sportu (2021).