The effects of laser energy deposition on supersonic cavity flow

Selin ARADAG, (TOBB Ekonomi ve Teknoloji Üniversitesi, Ankara, Türkiye)
Hong YAN, (Wright State Univercity Department, of Aerospace Engineering, Dayton Ohio, USA)
Doyle KNIGHT (Rutgers Univercity Department, of Mechanical and Aerospace Engineering, New Brunswick NJ, USA)
Isı Bilimi ve Tekniği Dergisi
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Yıl: 2009 Cilt: 29 Sayı: 2 Sayfa Aralığı: 67 - 73 Metin Dili: Türkçe İndeks Tarihi: 29-07-2022

The effects of laser energy deposition on supersonic cavity flow

Öz:
Bu çalışma, açık dikdörtgensel kaviteler üzerindeki basınç dalgalanmalarının lazer enerjisi ile azaltılmasının mümkün olup olmadığını araştıran sayısal bir çalışmadır. Simülasyonlar, enerji gönderilen ve gönderilmeyen iki ayrı durumda üç boyutlu bir kavite üzerindeki zamana bağlı değişen Mach sayısı 1.5 olan sesüstü akış için gerçekleştirilmiştir. Sıkıştırılabilir zamana bağlı Reynolds-ortalamalı Navier Stokes denklemleri üç boyutta GASPex adlı kod kullanarak çözümlenmiştir. Türbülans modeli olarak k-ω kullanılmıştır. Lazer enerjisini modellemek için Gauss sıcaklık profili kullanılmış, enerjinin gönderildiği noktadaki yoğunluğun başlangıçta uniform olduğu kabul edilmiştir. Çalışmada elde edilen sonuçlara göre, lazer enerjisi kavite içindeki akış yapısını değiştirerek, basınç dalgalanmalarını azaltmaktadır.
Anahtar Kelime:

Konular: Termodinamik

Lazer enerjisinin sesüstü kavitelerdeki akış üzerine etkileri

Öz:
The study examines the capability for reduction of the resonant pressure fluctuations in supersonic flow over an open rectangular cavity using repetitively pulsed energy deposition, computationally. The simulations are performed for the cases both with and without energy deposition for the unsteady flow over a three-dimensional cavity at a free stream Mach number of 1.5. The Reynolds-averaged compressible time dependent Navier Stokes equations in three dimensions are solved using the flow solver GASPex. The k-ω turbulence model is used. A Gaussian temperature profile is utilized to model the energy pulse assuming the density within the spot is initially uniform. The results indicate that energy deposition reduces the pressure fluctuations changing the flow structure within the cavity.
Anahtar Kelime:

Konular: Termodinamik
Belge Türü: Makale Makale Türü: Araştırma Makalesi Erişim Türü: Erişime Açık
  • Aerosoft Inc. General Aerodynamic Simulation Program User Manual, 1996.
  • Aradag, S., Yan, H. Knight, D., “Energy Deposition in Supersonic Cavity Flow", AIAA Paper No. 2004-0514, January 2004.
  • Bauer, R. C. and Dix, R. E., Engineering Model of Unsteady Flow in a Cavity, Calspan Corp./AEDC Operations, Arnold Engineering Development Center, TR-91-17, Tullahoma, TN, Dec. 1991.
  • Charwat, A. F., Roos, J. N., Dewey, Jr. F. C. and Hitz, J. A., An Investigation of Separated Flows-Part I: The Pressure Field, Journal of Aero. Sciences, Vol. 28, 1961, pp. 457-470.
  • Hankey, W. L. and Shang, J. S., The Numerical Solution to Pressure Oscillations in an Open Cavity, AIAA 79- 0136.
  • Heller, H. H., and Bliss, D. B., Physical Mechanism of Flow Induced Pressure Fluctuations in Cavities and Concepts for their Suppression, AIAA Paper 75-491, March 1975.
  • Kaufman, L. G., II, Maciulaitis, A. and Clark, R. L., Mach 0.6 to 3.0 Flows Over Rectangular Cavities, Air Force Wright Aeronautical Labs., AFWAL-TR-82-3112, May 1983.
  • Knight, D., Kuchinskiy, V., Kuranov, A., Sheikin, E., Survey of Aerodynamic Flow Control at High Speed by Energy Deposition, AIAA 2003-0525, 2003.
  • Lamp, A. M. and Chokani, N., Computation of Cavity Flows with Suppression Using Jet Blowing, Journal of Aircraft, Vol. 34, No. 4, July-August 1997.
  • Lazar, E., Elliott, G. Amd Glumac, N., “Control of the Shear Layer Above a Supersonic Cavity Using Energy Deposition”, AIAA Journal, vol. 46., No. 12, 2987- 2997, 2008.
  • Leu, Y. L, Dolling, D. S., Passive Control of Pressure Oscillations in Cavity Flow with Store Release, Confederation of European Aerospace Societies Forum on Wind Tunnels and Wind Tunnel Test Techniques, 1997.
  • Perng, S. W., Passive Control of Pressure Oscillations in Hypersonic Cavity Flow, Ph.D. Dissertation, Dept. of Aerospace Engineering and Engineering Mechanics, University of Texas at Austin, Austin, Texas, USA., 1996.
  • Rizzetta, D. P., Numerical Simulation of Supersonic Flow Over a Three-Dimensional Cavity, AIAA Journal, Vol. 26, No. 7, July 1988.
  • Rockwell, D. and Naudascher, E., Review-Selfsustaining Oscillations of Flow Past Cavities, ASME, Journal of Fluid Engr., Vol. 100, 1978, pp. 152-165.
  • Rossiter, J. E., Wind-Tunnel Experiments on the Flow Over Rectangular Cavities at Subsonic and Transonic speeds, A.R.C.R. & M., No. 3438, 1964.
  • Shih, S. H., Hamed, A. and Yeuan J. J., Unsteady Supersonic Cavity Flow Simulations Using Coupled k-ε and Navier-Stokes Equations, AIAA Journal, Vol. 32, No. 10, December 1994.
  • Stallings, R. L., Plentovich, E. B., Tracy, M. B., Hemsch, M. J., Effect of Passive Venting on Static Pressure Distributions in Cavities at Subsonic and Transonic Speeds, NASA Technical Memorandum 4549, June 1994.
  • Unalmis, O. H., Clemens, N. T. and Dolling, D. S., Planar Laser Imaging of a Supersonic Side-Facing Cavity, AIAA-99-0297.
  • Unalmis, O. H., Clemens, N.T. and Dolling, D.S., Planar Laser Imaging of High Speed Cavity Flow Dynamics,'AIAA-98-0776.
  • Wilcox, D. C., Turbulence Modeling For CFD, DCW Industries Inc., c1993.
  • Yan, H., Adelgren, R., Boguszko, M., Elliott, G., Knight, D., Laser Energy Deposition in Quiescent Air, AIAA Journal, Vol. 41, No. 10, pp. 1988--1995, 2003.
  • Zheltovodov and Yakovlev, V., Regimes of Separated FLows in Finite-Width Cavities and Methods of Their Control, in Separated Flows and Jets: IUTAM Symposium Novosibirsk/USSR 1990, Eds. Kozlov, V, and Dovgal, A., Springer-Verlag, Berlin, 1991, pp.529- 532.
APA ARADAG S, YAN H, KNIGHT D (2009). The effects of laser energy deposition on supersonic cavity flow. , 67 - 73.
Chicago ARADAG Selin,YAN Hong,KNIGHT Doyle The effects of laser energy deposition on supersonic cavity flow. (2009): 67 - 73.
MLA ARADAG Selin,YAN Hong,KNIGHT Doyle The effects of laser energy deposition on supersonic cavity flow. , 2009, ss.67 - 73.
AMA ARADAG S,YAN H,KNIGHT D The effects of laser energy deposition on supersonic cavity flow. . 2009; 67 - 73.
Vancouver ARADAG S,YAN H,KNIGHT D The effects of laser energy deposition on supersonic cavity flow. . 2009; 67 - 73.
IEEE ARADAG S,YAN H,KNIGHT D "The effects of laser energy deposition on supersonic cavity flow." , ss.67 - 73, 2009.
ISNAD ARADAG, Selin vd. "The effects of laser energy deposition on supersonic cavity flow". (2009), 67-73.
APA ARADAG S, YAN H, KNIGHT D (2009). The effects of laser energy deposition on supersonic cavity flow. Isı Bilimi ve Tekniği Dergisi, 29(2), 67 - 73.
Chicago ARADAG Selin,YAN Hong,KNIGHT Doyle The effects of laser energy deposition on supersonic cavity flow. Isı Bilimi ve Tekniği Dergisi 29, no.2 (2009): 67 - 73.
MLA ARADAG Selin,YAN Hong,KNIGHT Doyle The effects of laser energy deposition on supersonic cavity flow. Isı Bilimi ve Tekniği Dergisi, vol.29, no.2, 2009, ss.67 - 73.
AMA ARADAG S,YAN H,KNIGHT D The effects of laser energy deposition on supersonic cavity flow. Isı Bilimi ve Tekniği Dergisi. 2009; 29(2): 67 - 73.
Vancouver ARADAG S,YAN H,KNIGHT D The effects of laser energy deposition on supersonic cavity flow. Isı Bilimi ve Tekniği Dergisi. 2009; 29(2): 67 - 73.
IEEE ARADAG S,YAN H,KNIGHT D "The effects of laser energy deposition on supersonic cavity flow." Isı Bilimi ve Tekniği Dergisi, 29, ss.67 - 73, 2009.
ISNAD ARADAG, Selin vd. "The effects of laser energy deposition on supersonic cavity flow". Isı Bilimi ve Tekniği Dergisi 29/2 (2009), 67-73.
Sayfa Oluşturulma Tarihi
16-04-2024 21:24

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