Résumé of the AIAA FDTC Low Reynolds Number Discussion Group's canonical cases

48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition

Volumn , Issue , 2010, Pages

  Ol, Michael V ^a   Altman, Aaron ^b   Eldredge, Jeff D ^c   Garmann, Daniel J ^d   Lian, Yongsheng ^e  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b University of Dayton   (United States)

^c Engineering IV   (United States)

^d UNIVERSITY OF CINCINNATI   (United States)

^e University of Louisville   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACCELERATION EFFECTS; AERODYNAMIC FORCE COEFFICIENTS; BASELINE GEOMETRY; CLOSED-FORM MODELS; DOWNSTROKES; FLAT PLATE; GROUND TEST FACILITIES; GROWTH HISTORY; HIGH ACCELERATION; LEADING-EDGE VORTICES; LIFT COEFFICIENT; LOW REYNOLDS NUMBER; MOTION HISTORY; NUMERICAL COMPARISON; PARAMETER SPACES; PARAMETER VARIATION; PITCH MOTION; PIVOT POINT; QUASI-STEADY; REDUCED FREQUENCY; SHORT RUNS; TECHNICAL COMMITTEES; TIME HISTORY;

AEROSPACE ENGINEERING; AIRFOILS; LIFT; REYNOLDS NUMBER; WALLS (STRUCTURAL PARTITIONS);

FLIGHT DYNAMICS;

EID: 78649876245     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (15)

1. Drela, Mark. "XFOIL Subsonic Airfoil Development System." http://web.mit.edu/drela/Public/web/xfoil; 29 Jan. 2008.
2. Leishman, J.G. Principles of Helicopter Aerodynamics. Cambridge Aerospace Series, 2002.
3. Dickson, W.B., and Dickinson, M.H. "The Effect of Advance Ratio on the Aerodynamics of Revolving Wings". J. Exp. Bio., Vol. 207, pp. 4269-4281, 2007.
4. Lentink, D., and Dickinson, M.H. "Biofluiddynamic Scaling of Flapping, Spinning and Translating Fins and Wings". J. Exp. Bio., Vol. 212, pp. 2691-2704, 2009.
5. Visbal, M. "High-Fidelity Simulation of Transitional Flows past a Plunging Airfoil". AIAA 2009-0391.
6. Ol, M., Bernal, L., Kang, C.-K., and Shyy, W. "Shallow and Deep Dynamic Stall for Flapping Low Reynolds Number Airfoils". Experiments in Fluids, Vol. 46, Issue 5, pp. 883-901, May 2009.
7. Soria, J., and Kilany, K. "Multi-Component, Multi-Dimensional PIV measurements of Low Reynolds Number Flow around a Flat Plate Undergoing Pitch-Ramp Motion. AIAA 2009-3692.
8. Ol, M. "The High-Frequency, High-Amplitude Pitch Problem: Airfoils, Plates and Wings". AIAA 2009-3686.
9. Williams, D., Buntain, S., Quach, V., and Kerstens, W. "Flow Field Structures behind a 3D Wing in an Oscillating Freestream". AIAA 2009-3690.
10. Lian, Y. "Parametric Study of a Pitching Flat Plate at Low Reynolds Numbers". AIAA 2009-3688.
11. Garmann, D., and Visbal, M. "High Fidelity Simulations of Transitional Flow over Pitching Airfoils". AIAA 2009-3693.
12. Eldredge, J.D., Wang, C.J., and Ol, M. "A Computational Study of a Canonical Pitch-up, Pitch-down Wing Maneuver". AIAA 2009-3687.
13. Zheng, Z.C, Zhang, N, and Wei, Z. "Low-Reynolds Number Simulation for Flow over a Flapping Wing: Comparison to Measurement Data". AIAA 2009-3691.
14. Ol, M., Eldredge, J., and Wang, C. "High-Amplitude Pitch of a Flat Plate: an Abstraction of Perching and Flapping". Intl. J. MAVs, Vol. 1, No. 3, Sept. 2009.
15. Lian, Y., and Ol, M.V. "Experiments and Computation on a Low Aspect Ratio Pitching Flat Plate". AIAA 2010-0385.