Parametric PSE studies on distributed roughness laminar flow control

Collection of Technical Papers - 3rd AIAA Flow Control Conference

Volumn 3, Issue , 2006, Pages 1701-1710

  Atkin, C J ^a,c,d   Sunderland, R ^a,c   Mughal, M S ^b,e  

^a QINETIQ   (United Kingdom)

^b IMPERIAL COLLEGE LONDON   (United Kingdom)

^c Air Division (Aerodynamics Dept)   (United Kingdom)

^d AIAA   (United States)

^e Huxley Building ^*  (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

NONLINEAR STABILITY ANALYSIS; PRESSURE GRADIENTS; ROUGHNESS DISTRIBUTION;

FLOW CONTROL; FLOW VISUALIZATION; REYNOLDS NUMBER; SENSITIVITY ANALYSIS;

LAMINAR FLOW;

EID: 33845249692     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (12)

1. Saric W S, Carillo R B, Reibert M S. Leading-Edge Roughness as a Transition Control Mechanism. AIAA paper 98-0781, Reno, January 1998.
2. White E B, Saric W S. Application of Variable Leading-Edge Roughness for Transition Control on Swept Wings. AIAA paper 2000-0283, Reno, January 2000.
3. Saric W S, Reed H L. Toward Practical Laminar Flow Control - Remaining Challenges. AIAA paper 2004-2311, Portland, June 2004.
4. Atkin C J. Performance trade-off studies for a retrofit Hybrid Laminar Flow Control system. AIAA paper 2004-2215, Portland, June 2004.
5. Atkin C J, Mughal M S. Parametric Studies on the Application of Distributed Roughness Elements for Laminar Flow Control AIAA paper 2005-5263, 35th AIAA Fluid Dynamics Conference and Exhibit, Toronto, 6-9 June 2005, 2005.
6. Haynes T S, Reed H L. Simulation of swept-wing vortices using nonlinear parabolized stability equations. J. Fluid Mech. Vol. 405, pp. 325-349, 2000.
7. Somers D M, Horstmann K H. Design of a medium-speed natural-laminar-flow airfoil for commuter aircraft applications. DFVLR Report IB/29-85/26, 1985.
8. Ashill P R, Wood R F, Weeks D J. An improved, semi-inverse method of the viscous Garabedian and Korn method (VGK). RAETR 87002, 1987.
9. Atkin C J. Calculation of laminar boundary layers on swept-tapered wings. QinetiQ unpublished technical report, February 2004.
10. Atkin C J. User guide for CoDS version 3.3. DERA unpublished working paper, August 2001.
11. Mughal M S. Transition Prediction in Fully 3D Compressible Flows. Final report for QinetiQ contract CU002-8120, September 2001.
12. Herbert, T., Parabolized stability equations, AGARD R 793.4, 1994.