| Year |
Citation |
Score |
| 2018 |
Ramesh K, Granlund K, Ol MV, Gopalarathnam A, Edwards JR. Leading-edge flow criticality as a governing factor in leading-edge vortex initiation in unsteady airfoil flows Theoretical and Computational Fluid Dynamics. 32: 109-136. DOI: 10.1007/S00162-017-0442-0 |
0.504 |
|
| 2017 |
Medina A, Ol MV, Mancini P, Jones A. Revisiting Conventional Flaps at High Deflection Rate Aiaa Journal. 55: 2676-2685. DOI: 10.2514/1.J055754 |
0.434 |
|
| 2016 |
Granlund KO, Ol MV, Jones AR. Streamwise oscillation of airfoils into reverse flow Aiaa Journal. 54: 1628-1636. DOI: 10.2514/1.J054674 |
0.467 |
|
| 2015 |
Mancini PM, Jones AR, Granlund KO, Ol MV. Unsteady aerodynamic response of a rapidly started flexible wing International Journal of Micro Air Vehicles. 7: 147-158. DOI: 10.1260/1756-8293.7.2.147 |
0.479 |
|
| 2015 |
Mancini P, Manar F, Granlund K, Ol MV, Jones AR. Unsteady aerodynamic characteristics of a translating rigid wing at low Reynolds number Physics of Fluids. 27. DOI: 10.1063/1.4936396 |
0.528 |
|
| 2014 |
Granlund KO, Ol MV, Bernal LP. Free-to-pivot flat plates in hover for reynolds numbers 14 to 21, 200 Aiaa Journal. 52: 2083-2086. DOI: 10.2514/1.J053169 |
0.445 |
|
| 2014 |
Jantzen RT, Taira K, Granlund KO, Ol MV. Vortex dynamics around pitching plates Physics of Fluids. 26. DOI: 10.1063/1.4879035 |
0.493 |
|
| 2014 |
Granlund K, Monnier B, Ol M, Williams D. Airfoil longitudinal gust response in separated vs. attached flows Physics of Fluids. 26. DOI: 10.1063/1.4864338 |
0.495 |
|
| 2014 |
Ramesh K, Gopalarathnam A, Granlund K, Ol MV, Edwards JR. Discrete-vortex method with novel shedding criterion for unsteady aerofoil flows with intermittent leading-edge vortex shedding Journal of Fluid Mechanics. 751: 500-538. DOI: 10.1017/Jfm.2014.297 |
0.517 |
|
| 2014 |
Yu HT, Bernal LP, Granlund K, Ol MV. Aerodynamics of pitching wings: Theory and experiments 32nd Aiaa Applied Aerodynamics Conference. |
0.445 |
|
| 2014 |
Jantzen R, Taira K, Granlund K, Ol MV. Aerodynamic force modeling for unsteady wing maneuvers 52nd Aerospace Sciences Meeting. |
0.425 |
|
| 2013 |
Granlund KO, Ol MV, Bernal LP. Unsteady pitching flat plates Journal of Fluid Mechanics. 733. DOI: 10.1017/Jfm.2013.444 |
0.353 |
|
| 2013 |
Granlund K, Ol M, Bernal L. Quasi-steady response of free-to-pivot flat plates in hover Journal of Fluids and Structures. 40: 337-355. DOI: 10.1016/J.Jfluidstructs.2013.02.020 |
0.471 |
|
| 2013 |
Ramesh K, Gopalarathnam A, Edwards JR, Ol MV, Granlund K. An unsteady airfoil theory applied to pitching motions validated against experiment and computation Theoretical and Computational Fluid Dynamics. 27: 843-864. DOI: 10.1007/S00162-012-0292-8 |
0.501 |
|
| 2013 |
Ramesh K, Gopalarathnam A, Edwards JR, Granlund K, Ol MV. Theoretical analysis of perching and hovering maneuvers 31st Aiaa Applied Aerodynamics Conference. |
0.459 |
|
| 2013 |
Yu HT, Bernal LP, Ol MV. Effects of planform geometry and pivot axis location on the aerodynamics of pitching low aspect ratio wings 43rd Fluid Dynamics Conference. |
0.45 |
|
| 2013 |
Jantzen R, Taira K, Granlund K, Ol MV. On the in uence of pitching and acceleration on vortex dynamics around low-aspect-ratio rectangular wings 51st Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition 2013. |
0.398 |
|
| 2012 |
Gaston Z, Wan H, Dong H, Ol MV. Analysis of a hinge-connected flapping plate with an implemented torsional spring model 50th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. DOI: 10.2514/6.2012-298 |
0.345 |
|
| 2012 |
Baik YS, Bernal LP, Granlund K, Ol MV. Unsteady force generation and vortex dynamics of pitching and plunging aerofoils Journal of Fluid Mechanics. 709: 37-68. DOI: 10.1017/Jfm.2012.318 |
0.522 |
|
| 2012 |
Ramesh KK, Gopalarathnam A, Granlund K, Ol MV, Edwards JR. Theoretical modeling of leading edge vortices using the leading edge suction parameter 30th Aiaa Applied Aerodynamics Conference 2012. 1535-1551. |
0.42 |
|
| 2011 |
McGowan GZ, Granlund K, Ol MV, Gopalarathnam A, Edwards JR. Investigations of lift-based pitch-plunge equivalence for airfoils at low Reynolds numbers Aiaa Journal. 49: 1511-1524. DOI: 10.2514/1.J050924 |
0.475 |
|
| 2011 |
Ramesh K, Gopalarathnam A, Ol MV, Granlund K, Edwards JR. Augmentation of inviscid airfoil theory to predict and model 2D unsteady vortex dominated flows 41st Aiaa Fluid Dynamics Conference and Exhibit. |
0.425 |
|
| 2010 |
Yilmaz T, Ol M, Rockwell D. Scaling of flow separation on a pitching low aspect ratio plate Journal of Fluids and Structures. 26: 1034-1041. DOI: 10.1016/J.Jfluidstructs.2010.07.003 |
0.502 |
|
| 2010 |
Ol MV, Bernal L, Kang CK, Shyy W. Shallow and deep dynamic stall for flapping low Reynolds number airfoils Animal Locomotion. 321-339. DOI: 10.1007/S00348-009-0660-3 |
0.507 |
|
| 2010 |
Rausch JM, Baik YS, Bernal LP, Ol MV. Effect of aspect ratio on rigid lifting flat plates in pitch-plunge motion at low reynolds numbers 48th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. |
0.426 |
|
| 2010 |
Baik YS, Rausch JM, Bernal LP, Shyy W, Ol MV. Experimental study of governing parameters in pitching and plunging airfoil at low reynolds number 48th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. |
0.331 |
|
| 2010 |
Lian Y, Ol MV. Computation and experiments on a low aspect ratio pitching flat plate 48th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. |
0.43 |
|
| 2010 |
Baik YS, Aono H, Rausch JM, Bernal LP, Shyy W, Ol MV. Experimental study of a rapidly pitched flat plate at low reynolds number 40th Aiaa Fluid Dynamics Conference. |
0.481 |
|
| 2010 |
Rausch JM, Baik YS, Bernal LP, Cesnik CES, Shyy W, Ol MV. Fluid dynamics of flapping rigid and spanwise-flexible elliptical flat plates at low Reynolds numbers 40th Aiaa Fluid Dynamics Conference. |
0.375 |
|
| 2009 |
Ol MV, Eldredge JD, Wang C. High-Amplitude Pitch of a Flat Plate: An Abstraction of Perching and Flapping International Journal of Micro Air Vehicles. 1: 203-216. DOI: 10.1260/175682909789996186 |
0.527 |
|
| 2009 |
Ol MV, Reeder M, Fredberg D, McGowan GZ, Gopalarathnam A, Edwards JR. Computation vs. Experiment for High-Frequency Low-Reynolds Number Airfoil Plunge: International Journal of Micro Air Vehicles. 1: 99-119. DOI: 10.1260/175682909789498279 |
0.454 |
|
| 2009 |
Kang CK, Baik YS, Bernal L, Ol MV, Shyy W. Fluid dynamics of pitching and plunging airfoils of Reynolds number between 1×104 and 6×104 47th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. |
0.449 |
|
| 2009 |
Kang CK, Aono H, Trizila P, Baik Y, Rausch JM, Bernal L, Ol MV, Shyy W. Modeling of pitching and plunging airfoils at Reynolds number between 1×10 4 and 6×10 4 Collection of Technical Papers - Aiaa Applied Aerodynamics Conference. |
0.443 |
|
| 2009 |
Baik YS, Rausch JM, Bernal LP, Ol MV. Experimental investigation of pitching and plunging airfoils at reynolds number between 1×104 and 6×104 39th Aiaa Fluid Dynamics Conference. |
0.439 |
|
| 2009 |
Eldredge JD, Wang C, Ol MV. A computational study of a canonical pitch-up, pitch-down wing maneuver 39th Aiaa Fluid Dynamics Conference. |
0.448 |
|
| 2009 |
Alam MF, Suzen YB, Ol MV. Numerical simulations of pitching airfoil flowfields for MAV applications 39th Aiaa Fluid Dynamics Conference. |
0.39 |
|
| 2009 |
Baik YS, Rauschy JM, Bernal LP, Ol MV. Experimental investigation of pitching and plunging airfoils at reynolds number between 1×10 4 and 6×10 4 Collection of Technical Papers - Aiaa Applied Aerodynamics Conference. |
0.439 |
|
| 2009 |
Chabalko CC, Snyder RD, Beran PS, Ol MV. Study of deflected wake phenomena by 2D unsteady vortex lattice Collection of Technical Papers - Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference. |
0.319 |
|
| 2009 |
McGowan GZ, Gopalarathnam A, Ol MV, Edwards JR. Analytical, computational, and experimental investigations of equivalence between pitch and plunge motions for airfoils at low Reynolds numbers 47th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. |
0.37 |
|
| 2009 |
Ol MV. The high-frequency, high-amplitude pitch problem: Airfoils, plates and wings 39th Aiaa Fluid Dynamics Conference. |
0.439 |
|
| 2008 |
McGowan GZ, Gopalarathnam A, Ol MV, Edwards JR, Fredberg D. Computation vs. experiment for high-frequency low-Reynolds number airfoil pitch and plunge 46th Aiaa Aerospace Sciences Meeting and Exhibit. |
0.342 |
|
| 2008 |
Lian Y, Ol MV, Shyy W. Comparative study of pitch-plunge airfoil aerodynamics at transitional reynolds number 46th Aiaa Aerospace Sciences Meeting and Exhibit. |
0.339 |
|
| 2007 |
Kaplan SM, Altman A, Ol M. Wake vorticity measurements for low aspect ratio wings at low reynolds number Journal of Aircraft. 44: 241-251. DOI: 10.2514/1.23096 |
0.508 |
|
| 2007 |
Ol MV. Vortical structures in high frequency pitch and plunge at low reynolds number Collection of Technical Papers - 37th Aiaa Fluid Dynamics Conference. 2: 1696-1715. |
0.386 |
|
| 2006 |
Deluca AM, Reeder MF, Freeman J, Ol MV. Flexible- And rigid-wing micro air vehicle: Lift and drag comparison Journal of Aircraft. 43: 572-575. DOI: 10.2514/1.15643 |
0.318 |
|
| 2005 |
Ol MV, McAuliffe BR, Hanff ES, Scholz U, Kähler C. Comparison of laminar separation bubble measurements on a low Reynolds number airfoil in three facilities 35th Aiaa Fluid Dynamics Conference and Exhibit. |
0.362 |
|
| 2004 |
Khrabrov A, Ol MV. Effects of Flow Separation on Aerodynamic Loads in Linearized Thin Airfoil Theory Journal of Aircraft. 41: 944-948. DOI: 10.2514/1.5524 |
0.356 |
|
| 2003 |
Ol MV, Gharib M. Leading-Edge Vortex Structure of Nonslender Delta Wings at Low Reynolds Number Aiaa Journal. 41: 16-26. DOI: 10.2514/2.1930 |
0.577 |
|
| 2003 |
Ol MV, Gharib M. Leading-edge vortex structure of nonslender delta wings at low Reynolds number Aiaa Journal. 41: 16-26. |
0.45 |
|
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