| Year |
Citation |
Score |
| 2020 |
Ladeinde F. Reduced-Order Computational-Fluid-Dynamics-Based Analysis of Aviation Heat Exchangers Journal of Thermophysics and Heat Transfer. 1-20. DOI: 10.2514/1.T5903 |
0.349 |
|
| 2019 |
Ladeinde F, Alabi K, Li W. Optimization and Database Management in Smart Modeling of Aviation Heat Exchangers Journal of Thermophysics and Heat Transfer. 33: 1142-1152. DOI: 10.2514/1.T5733 |
0.527 |
|
| 2019 |
Ladeinde F, Lou Z, Li W. The effects of pressure treatment on the flamelet modeling of supersonic combustion Combustion and Flame. 204: 414-429. DOI: 10.1016/J.Combustflame.2019.03.030 |
0.576 |
|
| 2018 |
Ladeinde F, Li W. Differential Turbulent Supersonic Combustion of Hydrogen, Methane, and Ethylene, Without Assisted Ignition Aiaa Journal. 56: 4870-4883. DOI: 10.2514/1.J057124 |
0.511 |
|
| 2018 |
Ladeinde F, Kehinde A, Li W. Optimization of Heat Exchange in Manifold-Microchannel Grooves Journal of Heat Transfer-Transactions of the Asme. 140: 92403. DOI: 10.1115/1.4040141 |
0.498 |
|
| 2018 |
Ladeinde F, Cai X, Agarwal R. A methodology for hybrid simulation of rarefield and continuum flow regimes Aerospace Science and Technology. 75: 115-127. DOI: 10.1016/J.Ast.2017.12.036 |
0.47 |
|
| 2017 |
Ladeinde F, Lou Z. Improved Flamelet Modeling of Supersonic Combustion Journal of Propulsion and Power. 34: 750-761. DOI: 10.2514/1.B36779 |
0.348 |
|
| 2014 |
Zhan Y, Ladeinde F, Kirk HG, McDonald KT. The effects of pipe geometry on fluid flow in a muon collider particle production system Journal of Fluids Engineering, Transactions of the Asme. 136. DOI: 10.1115/1.4027176 |
0.602 |
|
| 2011 |
Li W, Ladeinde F. Analysis of interacting, underexpanded, rarefied jets Aiaa Journal. 49: 2581-2585. DOI: 10.2514/1.J050860 |
0.571 |
|
| 2011 |
Ladeinde F, Alabi K, Ladeinde T, Adamovich I, Gaitonde D. Advanced simulation and experiments on dynamic weakly-ionized plasma, with MHD and non-equilibrium chemistry 42nd Aiaa Plasmadynamics and Lasers Conference. |
0.715 |
|
| 2010 |
Ladeinde F. Advanced computational-fluid-dynamics techniques for scramjet combustion simulation Aiaa Journal. 48: 513-514. DOI: 10.2514/1.48989 |
0.337 |
|
| 2010 |
Ladeinde F, Alabi K, Ladeinde T, Davis D, Satchell M, Baurle RA. CFD enhancements for supersonic combustion simulation with VULCAN 46th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. |
0.693 |
|
| 2010 |
Ladeinde F, Alabi K, Colonius T, Gudmundsson K, Schlinker RH, Reba RA. An integrated RANS-PSE-wave packet tool for the prediction of subsonic and supersonic jet noise 16th Aiaa/Ceas Aeroacoustics Conference (31st Aiaa Aeroacoustics Conference). |
0.717 |
|
| 2008 |
Ladeinde F. Further development of a high-order prediction tool for combustion at all speeds 46th Aiaa Aerospace Sciences Meeting and Exhibit. |
0.309 |
|
| 2008 |
Ladeinde F, Cai X, Alabi K, Reba R, Schlinker RH, Simonich J. On the connection between near-field and far-field solutions of high-speed jet noise 46th Aiaa Aerospace Sciences Meeting and Exhibit. |
0.673 |
|
| 2008 |
Cai X, Ladeinde F. Performance of WENO scheme in generalized curvilinear coordinate systems 46th Aiaa Aerospace Sciences Meeting and Exhibit. |
0.346 |
|
| 2007 |
Cai X, Ladeinde F. A hybrid LES/RANS calculation of subsonic, supersonic hot jet noise Proceedings of the Asme Turbo Expo. 6: 1521-1530. DOI: 10.1115/GT2007-28117 |
0.302 |
|
| 2007 |
Alabi K, Ladeinde F. Utilizing CFD-based exergy calculations in the design/optimization of a complete aircraft system Collection of Technical Papers - 45th Aiaa Aerospace Sciences Meeting. 20: 13657-13671. |
0.701 |
|
| 2007 |
Cai X, Ladeinde F, Alabi K. Towards predicting supersonic, hot jet noise Collection of Technical Papers - 45th Aiaa Aerospace Sciences Meeting. 15: 10028-10043. |
0.714 |
|
| 2007 |
Alabi K, Ladeinde F, VonSpakovsky M, Moorhouse D, Camberos J. An advanced exergy and energy simulation tool for large-scale design/optimization of aerospace systems Collection of Technical Papers - 39th Aiaa Thermophysics Conference. 1: 465-481. |
0.689 |
|
| 2007 |
Alabi K, Ladeinde F. High-order dynamic overset procedure applied to moving body calculations Collection of Technical Papers - 45th Aiaa Aerospace Sciences Meeting. 5: 2904-2920. |
0.696 |
|
| 2007 |
Safta C, Ladeinde F, Cai X, Alabi K. A combined level-set/mixture fraction/progress-variable approach for partially-premixed turbulent reacting flows Collection of Technical Papers - 45th Aiaa Aerospace Sciences Meeting. 24: 16950-16956. |
0.75 |
|
| 2006 |
Alabi K, Ladeinde F, Von Spakovsky M, Moorhouse D, Camberos J. The use of the 2nd law as a potential design tool for aircraft air frame subsystems International Journal of Thermodynamics. 9: 193-205. DOI: 10.5541/Ijot.1034000182 |
0.738 |
|
| 2006 |
Safta C, Alabi K, Ladeinde F, Cai X, Kiel B, Sekar B. Level-set flamelet/large-eddy simulation of a premixed augmentor flame holder Collection of Technical Papers - 44th Aiaa Aerospace Sciences Meeting. 3: 1882-1897. |
0.734 |
|
| 2006 |
Alabi K, Ladeinde F, Von Spakovsky M, Moorhouse D, Camberos J. Assessing CFD modeling of entropy generation for the air frame subsystem in an integrated aircraft design/synthesis procedure Collection of Technical Papers - 44th Aiaa Aerospace Sciences Meeting. 10: 7036-7054. |
0.728 |
|
| 2006 |
Ladeinde F, Alabi K, Safta C, Cai X, Johnson F. The first high-order CFD simulation of aircraft: Challenges and opportunities Collection of Technical Papers - 44th Aiaa Aerospace Sciences Meeting. 24: 18161-18183. |
0.725 |
|
| 2006 |
Safta C, Ladeinde F, Cai X, Alabi K. A high-fidelity level-set flamelet approach for predicting turbulent reacting flows Collection of Technical Papers - Aiaa/Asme/Sae/Asee 42nd Joint Propulsion Conference. 9: 7361-7373. |
0.744 |
|
| 2006 |
Alabi K, Ladeinde F. The implementation of influence boundary procedures in CFD Collection of Technical Papers - 44th Aiaa Aerospace Sciences Meeting. 17: 13144-13168. |
0.7 |
|
| 2006 |
Cai X, Ladeinde F. An evaluation of the partially-resolved numerical simulation procedure for near-wall turbulence prediction Collection of Technical Papers - 44th Aiaa Aerospace Sciences Meeting. 3: 1456-1468. |
0.354 |
|
| 2006 |
Safta C, Alabi K, Ladeinde F. Comparative advantages of high-order schemes for subsonic, transonic, and supersonic flows Collection of Technical Papers - 44th Aiaa Aerospace Sciences Meeting. 5: 3567-3586. |
0.717 |
|
| 2005 |
Alabi K, Ladeinde F. Direct numerical simulation of the effects of upstream turbulence on flow over aircraft engine turbine blades 43rd Aiaa Aerospace Sciences Meeting and Exhibit - Meeting Papers. 7863-7877. |
0.748 |
|
| 2005 |
Alabi K, Ladeinde F. Treatment of blank nodes in a high-order overset procedure 43rd Aiaa Aerospace Sciences Meeting and Exhibit - Meeting Papers. 15145-15153. |
0.695 |
|
| 2004 |
Choi J, Teng S, Han JC, Ladeinde F. Effect of free-stream turbulence on turbine blade heat transfer and pressure coefficients in low Reynolds number flows International Journal of Heat and Mass Transfer. 47: 3441-3452. DOI: 10.1016/J.Ijheatmasstransfer.2004.01.015 |
0.423 |
|
| 2004 |
Ladeinde F, Cai X, Li W, Agarwall R. A unified computational methodology for rarefied and continuum flow regimes Aiaa Paper. 7741-7775. |
0.359 |
|
| 2004 |
Alabi K, Ladeinde F. Parallel, high-order overset grid implementation for supersonic flows Aiaa Paper. 706-731. |
0.744 |
|
| 2002 |
Ladeinde F. Direct simulation of compressible MHD turbulence 33rd Plasmadynamics and Lasers Conference. |
0.335 |
|
| 2001 |
Ladeinde F, Cai X, Visbal MR, Gaitonde DV. Turbulence spectra characteristics of high order schemes for direct and large eddy simulation Applied Numerical Mathematics. 36: 447-474. DOI: 10.1016/S0168-9274(00)00019-2 |
0.37 |
|
| 2001 |
Ladeinde F, Cai X, Sekar B, Kiel B. Application of combined LES and Flamelet modeling to Methane, Propane, and Jet-A Combustion 39th Aerospace Sciences Meeting and Exhibit. |
0.324 |
|
| 1998 |
Ladeinde F, Liu W, O'Brien EE. Turbulence in compressible mixing layers Journal of Fluids Engineering, Transactions of the Asme. 120: 48-53. DOI: 10.1115/1.2819659 |
0.425 |
|
| 1997 |
Cai XD, O'Brien EE, Ladeinde F. Thermodynamic behavior in decaying, compressible turbulence with initially dominant temperature fluctuations Physics of Fluids. 9: 1754-1763. DOI: 10.1063/1.869292 |
0.378 |
|
| 1997 |
Ladeinde F, Nearon MD. Proper simulation of convective, turbulent rotating flows American Society of Mechanical Engineers, Fluids Engineering Division (Publication) Fed. 14. |
0.309 |
|
| 1997 |
Ladeinde F, Liu W, O'Brien EE. DNS studies of turbulence in compressible mixing layers American Society of Mechanical Engineers, Fluids Engineering Division (Publication) Fed. 15. |
0.321 |
|
| 1996 |
Ladeinde F, O'Brien EE, Cai XD. A parallelized eno procedure for direct numerical simulation of compressible turbulence Journal of Scientific Computing. 11: 179-205. |
0.304 |
|
| 1995 |
Ladeinde F. Supersonic flux-split procedure for second moments of turbulence Aiaa Journal. 33: 1185-1195. DOI: 10.2514/3.12544 |
0.431 |
|
| 1995 |
Ladeinde F, Intile JC. Calculation of Reynolds stresses in turbulent supersonic flows International Journal For Numerical Methods in Fluids. 21: 49-74. DOI: 10.1002/Fld.1650210105 |
0.452 |
|
| 1995 |
Ladeinde F, O'Brien EE, Cai X, Liu W. Advection by polytropic compressible turbulence Physics of Fluids. 7: 2848-2857. |
0.344 |
|
| 1994 |
Ladeinde F, Akay HU. The calculation of scalar transport during the injection molding of thermoset polymers Applied Mathematical Modelling. 18: 347-357. DOI: 10.1016/0307-904X(94)90359-X |
0.327 |
|
| 1991 |
Ladeinde F, Torrance KE. Convection in a rotating, horizontal cylinder with radial and normal gravity forces Journal of Fluid Mechanics. 228: 361-385. DOI: 10.1017/S0022112091002744 |
0.543 |
|
| 1990 |
Ladeinde F, Torrance KE. Galerkin finite element simulation of convection driven by rotation and gravitation International Journal For Numerical Methods in Fluids. 10: 47-77. DOI: 10.1002/Fld.1650100105 |
0.619 |
|
| 1990 |
Ladeinde F, Torrance KE. Transient plumes from convective flow instability in horizontal cylinders Journal of Thermophysics and Heat Transfer. 4: 350-356. |
0.601 |
|
| Show low-probability matches. |
