Experimental and Computational Study of Underexpanded Jet Impingement Heat Transfer
作者： Shann Rufer , Robert Nowak , Kamran Daryabeigi , Donald Picetti
DOI: 10.2514/6.2009-4311
关键词:
摘要: An experiment was performed to assess CFD modeling of a hypersonic-vehicle breach, boundary-layer flow ingestion and internal surface impingement. Tests were conducted in the NASA Langley Research Center 31-Inch Mach 10 Tunnel. Four simulated breaches tested impingement heat flux data obtained for each case using both phosphor thermography thin film gages on targets placed inside model. A separate target used measure pressure distribution. The measured jet width peak location are good agreement with analysis.
handle.net参考文章(20)
Steven W. Smith, Digital Signal Processing: A Practical Guide for Engineers and Scientists ,(2002)
Brian R. Hollis, User's manual for the one-dimensional hypersonic experimental aero-thermodynamic (1DHEAT) data reduction code NASA STI/Recon Technical Report N. ,vol. 96, pp. 16042- ,(1995)
Jennifer Ann Inman, Fluorescence imaging study of free and impinging supersonic jets: Jet structure and turbulent transition PhDT. ,(2007) , 10.21220/S2-WMWX-9G76
P. A. Gnoffo, J. R. Micol, C. G. Miller, Laminar heat-transfer distributions on biconics at incidence in hypersonic-hypervelocity flows STIN. ,vol. 85, pp. 16065- ,(1984)
Gregory M. Buck, Automated thermal mapping techniques using chromatic image analysis STIN. ,vol. 89, pp. 25443- ,(1989)
Jennifer Wilkes, Christopher Glass, Paul Danehy, Robert Nowak, Fluorescence Imaging of Underexpanded Jets and Comparison with CFD 44th AIAA Aerospace Sciences Meeting and Exhibit. ,(2006) , 10.2514/6.2006-910
C. G. Miller, Comparison of thin-film resistance heat-transfer gages with thin-skin transient calorimeter gages in conventional hypersonic wind tunnels NASA STI/Recon Technical Report N. ,vol. 82, pp. 14474- ,(1981)
Dale Arden Anderson, Computational Fluid Mechanics and Heat Transfer ,(1984)
Michael J. Wright, Graham V. Candler, Deepak Bose, Data-Parallel Line Relaxation Method for the Navier -Stokes Equations AIAA Journal. ,vol. 36, pp. 1603- 1609 ,(1998) , 10.2514/2.586
John R. Micol, Langley Aerothermodynamic Facilities Complex: Enhancements and Testing Capabilities 36th AIAA Aerospace Sciences Meeting and Exhibit. ,(1998) , 10.2514/6.1998-147