Year |
Citation |
Score |
2020 |
Fujiwara GEC, Bragg MB, Broeren AP. Comparison of Computational and Experimental Ice Accretions of Large Swept Wings Journal of Aircraft. 57: 342-359. DOI: 10.2514/1.C035631 |
0.807 |
|
2019 |
Stebbins SJ, Loth E, Broeren AP, Potapczuk M. Review of computational methods for aerodynamic analysis of iced lifting surfaces Progress in Aerospace Sciences. 111: 100583. DOI: 10.1016/J.Paerosci.2019.100583 |
0.621 |
|
2017 |
Broeren AP, Addy HE, Lee S, Monastero MC, McClain ST. Three-Dimensional Ice-Accretion Measurement Methodology for Experimental Aerodynamic Simulation Journal of Aircraft. 55: 817-828. DOI: 10.2514/1.C034580 |
0.835 |
|
2016 |
Broeren AP, Lee S, Clark C. Aerodynamic effects of anti-icing fluids on a thin high-performance wing section Journal of Aircraft. 53: 451-462. DOI: 10.2514/1.C033384 |
0.759 |
|
2016 |
Broeren AP, Potapczuk MG, Lee S, Malone AM, Paul BP, Woodard BS. Ice-accretion test results for three large-scale swept-wing models in the NASA icing research tunnel 8th Aiaa Atmospheric and Space Environments Conference. |
0.749 |
|
2015 |
König B, Fares E, Broeren AP. Lattice-Boltzmann Analysis of Three-Dimensional Ice Shapes on a NACA 23012 Airfoil Sae Technical Papers. 2015. DOI: 10.4271/2015-01-2084 |
0.694 |
|
2013 |
Addy HE, Broeren AP, Oleskiw M, Orchard D. A study of the effects of altitude on thermal ice protection system performance 5th Aiaa Atmospheric and Space Environments Conference. DOI: 10.2514/6.2013-2934 |
0.601 |
|
2013 |
Broeren AP, Lee S, Clark C. Aerodynamic characterization of a thin, high-performance airfoil for use in ground fluids testing 5th Aiaa Atmospheric and Space Environments Conference. DOI: 10.2514/6.2013-2933 |
0.683 |
|
2013 |
Diebold JM, Broeren AP, Bragg MB. Aerodynamic classification of swept-wing ice accretion 5th Aiaa Atmospheric and Space Environments Conference. DOI: 10.2514/6.2013-2825 |
0.8 |
|
2013 |
Broeren AP, Potapczuk MG, Riley JT, Villedieu P, Moëns F, Bragg MB. Swept-wing ice accretion characterization and aerodynamics 5th Aiaa Atmospheric and Space Environments Conference. DOI: 10.2514/6.2013-2824 |
0.826 |
|
2013 |
Broeren AP, Riley JT. Scaling of lift degradation due to antiicing fluids Journal of Aircraft. 50: 1886-1895. DOI: 10.2514/1.C032259 |
0.489 |
|
2013 |
Broeren AP, Addy HE, Lee S, Monastero MC. Validation of 3-D ice accretion measurement methodology for experimental aerodynamic simulation Transactions of Japanese Society For Medical and Biological Engineering. 51. |
0.716 |
|
2013 |
Lee S, Broeren AP, Kreeger RE, Potapczuk M, Utt L. Implementation and validation of 3-D ice accretion measurement methodology Transactions of Japanese Society For Medical and Biological Engineering. 51. |
0.636 |
|
2012 |
Broeren AP, Riley JT. Scaling of lift degradation due to anti-icing fluids based upon the aerodynamic Acceptance test 4th Aiaa Atmospheric and Space Environments Conference 2012. |
0.561 |
|
2012 |
Lee S, Broeren AP, Addy HE, Sills R, Pifer EM. Development of 3D ice accretion measurement method 4th Aiaa Atmospheric and Space Environments Conference 2012. |
0.538 |
|
2011 |
Broeren AP, Lee S, Shah GH, Murphy PC. Aerodynamic effects of simulated ice accretion on a generic transport model Sae Technical Papers. DOI: 10.4271/2011-38-0065 |
0.729 |
|
2010 |
Broeren AP, Whalen EA, Busch GT, Bragg MB. Aerodynamic simulation of runback ice accretion Journal of Aircraft. 47: 924-939. DOI: 10.2514/1.46475 |
0.809 |
|
2010 |
Broeren AP, Bragg MB, Addy HE, Lee S, Moens F, Guffond D. Effect of high-fidelity ice-accretion simulations on full-scale airfoil performance Journal of Aircraft. 47: 240-254. DOI: 10.2514/1.45203 |
0.879 |
|
2009 |
DeSalle DC, Gilliot A, Geiler C, Monnier JC, Broeren AP, Addy HE. Experimental investigations of simulated ice accretions at high reynolds numbers in the ONERA F1 wind tunnel 1st Aiaa Atmospheric and Space Environments Conference. |
0.745 |
|
2008 |
Busch GT, Broeren AP, Bragg MB. Aerodynamic simulation of a horn-ice accretion on a subscale model Journal of Aircraft. 45: 604-613. DOI: 10.2514/1.32338 |
0.831 |
|
2008 |
Whalen EA, Broeren AP, Bragg MB. Aerodynamics of scaled runback ice accretions Journal of Aircraft. 45: 591-603. DOI: 10.2514/1.32274 |
0.858 |
|
2008 |
Broeren AP, Bragg MB, Addy HE, Lee S, Moens F, Guffond D. Effect of high-fidelity ice accretion simulations on the performance of a full-scale airfoil model 46th Aiaa Aerospace Sciences Meeting and Exhibit. |
0.852 |
|
2007 |
Broeren AP, Busch GT, Bragg MB. Aerodynamic fidelity of ice accretion simulation on a subscale model Sae Technical Papers. DOI: 10.4271/2007-01-3285 |
0.853 |
|
2007 |
Campbell SE, Broeren AP, Bragg MB. Sensitivity of aircraft performance to icing parameter variations Journal of Aircraft. 44: 1758-1760. DOI: 10.2514/1.32355 |
0.852 |
|
2007 |
Campbell SE, Broeren AP, Bragg MB, Miller DR. Aircraft performance sensitivity to icing cloud conditions Collection of Technical Papers - 45th Aiaa Aerospace Sciences Meeting. 2: 989-1005. |
0.814 |
|
2006 |
Broeren AP, Bragg MB, Addy HE. Flowfield measurements about an airfoil with leading-edge ice shapes Journal of Aircraft. 43: 1226-1234. DOI: 10.2514/1.19021 |
0.816 |
|
2006 |
Broeren AP, Bragg MB. Aerodynamics of ice remnants from protected surfaces Collection of Technical Papers - 44th Aiaa Aerospace Sciences Meeting. 5: 3149-3169. |
0.841 |
|
2006 |
Whalen EA, Broeren AP, Bragg MB. Considerations for aerodynamic testing of scaled runback ice accretions Collection of Technical Papers - 44th Aiaa Aerospace Sciences Meeting. 5: 3170-3185. |
0.86 |
|
2006 |
Blumenthal LA, Busch GT, Broeren AP, Bragg MB. Issues in ice accretion aerodynamic simulation on a subscale model Collection of Technical Papers - 44th Aiaa Aerospace Sciences Meeting. 5: 3200-3219. |
0.846 |
|
2005 |
Broeren AP, Bragg MB. Effect of airfoil geometry on performance with simulated intercycle ice accretions Journal of Aircraft. 42: 121-130. DOI: 10.2514/1.4734 |
0.864 |
|
2005 |
Bragg MB, Broeren AP, Blumenthal LA. Iced-airfoil aerodynamics Progress in Aerospace Sciences. 41: 323-362. DOI: 10.1016/J.Paerosci.2005.07.001 |
0.799 |
|
2005 |
Whalen EA, Broeren AP, Bragg MB, Lee S. Characteristics of runback ice accretions on airfoils and their aerodynamic effects 43rd Aiaa Aerospace Sciences Meeting and Exhibit - Meeting Papers. 207-220. |
0.858 |
|
2005 |
Broeren AP, Bragg MB. Effect of airfoil geometry on performance with simulated intercycle ice accretions Journal of Aircraft. 42: 121-130. |
0.764 |
|
2005 |
Broeren AP, LaMarre CM, Bragg MB, Lee S. Characteristics of SLD ice accretions on airfoils and their aerodynamic effects 43rd Aiaa Aerospace Sciences Meeting and Exhibit - Meeting Papers. 3027-3050. |
0.841 |
|
2004 |
Broeren AP, Bragg MB, Addy HE. Effect of Intercycle Ice Accretions on Airfoil Performance Journal of Aircraft. 41: 165-174. DOI: 10.2514/1.1683 |
0.839 |
|
2004 |
Broeren AP, Bragg MB, Addy HE. Effect of Intercycle Ice Accretions on Airfoil Performance Journal of Aircraft. 41: 165-174. |
0.731 |
|
2003 |
Bragg MB, Broeren AP, Blumenthal LA. Iced-airfoil and wing aerodynamics Sae Technical Papers. DOI: 10.4271/2003-01-2098 |
0.8 |
|
2003 |
Addy HE, Broeren AP, Zoeckler JG, Lee S. A wind tunnel study of icing effects on a business jet airfoil 41st Aerospace Sciences Meeting and Exhibit. |
0.712 |
|
2001 |
Broeren AP, Bragg MB. Spanwise variation in the unsteady stalling flowfields of two-dimensional airfoil models 39th Aerospace Sciences Meeting and Exhibit. DOI: 10.2514/2.1501 |
0.589 |
|
2001 |
Anderson DN, Botura GC, Broeren AP. A study of scaling for Intercycle ice accretion tests 39th Aerospace Sciences Meeting and Exhibit. |
0.662 |
|
1999 |
Broeren AP, Bragg MB. Flowfield measurements over an airfoil during natural low-frequency oscillations near stall Aiaa Journal. 37: 130-132. DOI: 10.2514/2.678 |
0.498 |
|
1998 |
Broeren AP, Bragg MB. Low-frequency flowfield unsteadiness during airfoil stall and the influence of stall type 16th Aiaa Applied Aerodynamics Conference. 196-209. |
0.553 |
|
1996 |
Broeren AP, Bragg MB. Phase-averaged ldv flowfield measurements about an airfoil in unsteady stall 14th Applied Aerodynamics Conference. 921-931. |
0.544 |
|
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