Otwarty dostęp

Quantitative Visualisation of Compressible Flows


Zacytuj

[1] Anderson J.D., 2004, “Fundamentals of Aerodynamics”, 5th edition, McGraw-Hill’s Search in Google Scholar

[2] Galinski C. and Goraj Z., 2004, “Experimental and numerical results obtained for a scaled RPV and a full size aircraft”, Aircraft Engineering and Aerospace Technology, No. 76, pp. 305-313.10.1108/00022660410536041 Search in Google Scholar

[3] Żółtak J. and Stalewski W., 2014, “Preliminary Design of the Air-Intake System and the Nacelle in the Small Aircraft-Engine Integration Process”, Aircraft Engineering and Aerospace Technology, No. 86, pp. 250-258.10.1108/AEAT-01-2013-0015 Search in Google Scholar

[4] Lee B.H.K., 1989, “Investigation of flow separation on a supercritical airfoil”, Journal of Aircraft, No. 26, pp. 1032-1039.10.2514/3.45876 Search in Google Scholar

[5] Adrian R.J., 1991, “Particle-imaging techniques for experimental fluid mechanics”, Annual Review of Fluid Mechanics, No. 23, pp. 261-304.10.1146/annurev.fl.23.010191.001401 Search in Google Scholar

[6] Wilert C.E., Gharib M., 1991, “Digital particle image velocimetry”, Experiments in Fluids, No. 10, pp. 181-193.10.1007/BF00190388 Search in Google Scholar

[7] Parsad A.K., 2000, “Stereoscopic particle image velocimetry”, Experiments in Fluids, No. 29, pp. 103-116.10.1007/s003480000143 Search in Google Scholar

[8] Scarano F., 2013, “Tomographic PIV: principles and practice”, Measurement Science and Technology, No. 24, pp. 1-28.10.1088/0957-0233/24/1/012001 Search in Google Scholar

[9] Raffel M., 2015, “Background-oriented schlieren (BOS) techniques”, Experiments in Fluids, No. 56, p. 60.10.1007/s00348-015-1927-5 Search in Google Scholar

[10] Stryczniewicz W. 2012, “Development of Particle Image Velocimetry Algorithm”, Problems of Mechatronics, No. 9, pp. 41-54. Search in Google Scholar

[11] Venkatakrishnan L., Meier G.E.A., 2004, “Density measurements using the Background Oriented Schlieren technique”, Experiments in Fluids, No. 37, pp. 237-247.10.1007/s00348-004-0807-1 Search in Google Scholar

[12] Manovski P., Wehrmeyer J., Scott K., Loxton B., Quick H., Lam S. and Giacobello M., 2016, “A Performance Comparison between Classical Schlieren and Background-Oriented Schlieren”, 18th International Symposium on the Application of Laser and Imaging Techniques to Fluid Mechanics, Lisbon, June 04-07. Search in Google Scholar

[13] Clem M.M., Zamam K.B.M.Q. and Fagan A. F., 2012, “Background Oriented Schlieren Applied to Study Shock Spacing in a Screeching Circular Jet”, 50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Nashville, January 09-12.10.2514/6.2012-403 Search in Google Scholar

[14] Heineek J. T., Banks D. W., Schairer E. T., Haering E. A. and Bean P. S., 2016, “Background Oriented Schlieren (BOS) of a Supersonic Aircraft in Flight”, AIAA Flight Testing Conference, Washington D.C., June 13-17.10.2514/6.2016-3356 Search in Google Scholar

[15] Bauknecht A., Merz C.B. and Raffel M., 2014, “Airborne Application of the Background Oriented Schlieren Technique to a Helicopter in Forward Flight”, 17th International Symposium on the Application of Laser and Imaging Techniques to Fluid Mechanics, Lisbon, June 07-10. Search in Google Scholar

[16] Raffel M., Willert C.E., Wereley S.T. and Kompenhans J., 2007, “Particle Image Velocimetry, a practical guide”. 2nd edition, Springer-Verlag.10.1007/978-3-540-72308-0 Search in Google Scholar

[17] Surmacz K., Ruchała P and Stryczniewicz W., 2016, “Wind tunel tests of the developement and demise of Vortex Ring State of the rotor”. In Kleiber Advances in Mechanics: Theoretical, Computational and Interdisciplinary Issues, CRC Press.10.1201/b20057-118 Search in Google Scholar

[18] Urban J.M., Zloczewska A, Stryczniewicz W, and Jönsson-Niedziolka M., 2013, “Enzymatic oxygen reduction under quiescent conditions – The importance of convection”, Electrochemistry Communications, No. 34, pp. 94-97.10.1016/j.elecom.2013.05.030 Search in Google Scholar

[19] Jun Z., Zhenghong G., Hao Z. and Junqiang B., 2009, “A high-speed nature laminar flow airfoil and its experimental study in wind tunnel with nonintrusive measurement technique”, Chinese Journal of Aeronautics, No. 22, pp. 225-229.10.1016/S1000-9361(08)60091-6 Search in Google Scholar

[20] Raffel M. and Kompenhaus J., 1993, “PIV measurements of unsteady transonic flow fields above a NACA 0012 airfoil”, Laser Anemometry Advances and Applications, No. 2052, pp. 527-534.10.1117/12.150547 Search in Google Scholar

[21] Giepman R.H.M., Schrijer F.F.J. and van Oudheusden B. W., 2015, “High-resolution PIV measurements of a transitional shock”, Experiments in Fluids, No. 56, pp. 113-133.10.1007/s00348-015-1977-8 Search in Google Scholar

[22] Hartmann A., Klaas M. and Schröder W., 2010, “Time resolved stereo PIV measurements of unsteady shock-boundary layer interaction on a supercritical airfoil”, 15th Int Symposium on Applications of Laser Techniques to Fluid Mechanics, Lisbon, July 5-8. Search in Google Scholar

[23] Wiśniowski W., 2014, “Specializations of the Institute of Aviation – review and conclusions”, Transactions of the Institute of Aviation, No. 235, pp 7-16.10.5604/05096669.1130233 Search in Google Scholar

[24] Stryczniewicz W. and Surmacz K., 2014, “PIV Measurements of the Vortex Ring State of the Main Rotor of a Helicopter”, Transactions of the Institute of Aviation, No. 235, pp. 17-27.10.5604/05096669.1130234 Search in Google Scholar

[25] McDevitt J.B., Levy L.L. Jr. and Deiwert G. S., 1976, “Transonic Flow About a Thick Circular-Arc Airfoil”, AIAA Journal, No. 14, pp. 606-613.10.2514/3.61402 Search in Google Scholar

[26] Mundell A.R.G. and Mabey D.G., 1986, “Pressure fluctuations caused by transonic shock/boundary-layer interaction”, Aeronautical Journal, No. 90, pp. 274-282.10.1017/S0001924000015864 Search in Google Scholar

eISSN:
2545-2835
Język:
Angielski
Częstotliwość wydawania:
4 razy w roku
Dziedziny czasopisma:
Engineering, Introductions and Overviews, other, Geosciences, Materials Sciences, Physics