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© Numerical Simulation Of Surface Heat Transfer From An Array Of Hot-Air Jets Saeed, F AMER INST AERONAUT ASTRONAUT, JOURNAL OF AIRCRAFT; pp: 700-714;

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Presentation on theme: "© Numerical Simulation Of Surface Heat Transfer From An Array Of Hot-Air Jets Saeed, F AMER INST AERONAUT ASTRONAUT, JOURNAL OF AIRCRAFT; pp: 700-714;"— Presentation transcript:

1 © Numerical Simulation Of Surface Heat Transfer From An Array Of Hot-Air Jets Saeed, F AMER INST AERONAUT ASTRONAUT, JOURNAL OF AIRCRAFT; pp: 700-714; Vol: 45 King Fahd University of Petroleum & Minerals http://www.kfupm.edu.sa Summary A numerical study was conducted to simulate the heat transfer from an array of jets onto an impingement surface typical of those found on aircraft wing/slat surfaces. The study used the commercially available computational fluid dynamics software FLUENT to model the different hot-jet arrangements that included 1) a single array of jets, 2) two staggered arrays of jets at different stagger angles (10 and 20 degrees), and 3) a case with an etched surface. The main findings of the study reveal that the single array and the array with a 20 degree stagger yield better surface heat transfer than the 10 degree stagger. The etched surface or inner liner yields almost 2-3 times better surface heat transfer than the others, thus making it a favorable choice for increasing surface heat transfer. References: 1. 2002, GAMBIT 2 USERS GUIDE 2. *FAA, 1997, INFL IC PLAN 3. *FED AV ADM, 1996, P FAA INT C AIRCR IN 4. *FLUENT, 2002, FLUENG 6 US GUID 5. *PHOENICS, 2000, PHOENICS CFD COD 6. ALKHALIL KM, 1991, THESIS U TOLEDO TOLE 7. ALKHALIL KM, 1996, 31 AER SCI M EXH 8. ALKHALIL KM, 1997, 35 AER SCI M EXH 9. BROWN JM, 2002, J AIRCRAFT, V39, P65 10. CORNARO C, 1999, EXP THERM FLUID SCI, V20, P66 11. CROCE G, 1998, 36 AER SCI M EXH 12. CROCE G, 2002, 200386 AIAA 13. DYBAN EP, 1969, INZHENERNO FIZICHESK, V17, P785 Copyright: King Fahd University of Petroleum & Minerals; http://www.kfupm.edu.sa

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