Applied computational aerodynamics : a modern engineering approach /Author: Cummings, Russell M.
Publisher: New York, NY : Cambridge University Press,
Date: 2015. This title can be found in 1 Iowa libraries.
Applications of circulation control technologies /Publisher: Reston, VA : American Institute of Aeronautics and Astronautics,
Date: c2006. This title can be found in 1 Iowa libraries.
Analysis of low-speed unsteady airfoil flows /Publisher: Berlin : Springer, Berlin : Springer,
Date: c2005. This title can be found in 1 Iowa libraries.
Computational study of large droplet breakup in the vicinity of an airfoil final report.Format: [electronic resource] :
Publisher: Washington, D.C. : U.S. Dept. of Transportation, Federal Aviation Administration, Office of Aviation Research,
Date: [2005] This title can be found in 1 Iowa libraries.
Wind turbine post-stall airfoil performance characteristics guidelines for blade-element momentum methods preprint /Format: [electronic resource] :
Author: Tangler, James L.
Publisher: Golden, Colo. : National Renewable Energy Laboratory,
Date: [2004] This title can be found in 2 Iowa libraries.
LESFOIL : large eddy simulation of flow around a high lift airfoil : results of the Project LESFOIL supported by the European Union, 1998-2001 /Publisher: New York : New York : Springer,
Date: c2003. This title can be found in 2 Iowa libraries.
An experimental and computational investigation of oscillating airfoil unsteady aerodynamics at large mean incidenceFormat: [microform] /
Author: Capece, Vincent R.
Publisher: [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ;
Date: 2003] This title can be found in 1 Iowa libraries.
Transient growth theory prediction of optimal placing of passive and active flow control devices for separation delay in LPT airfoilsFormat: [microform] /
Author: Tumin, A. M.
Publisher: [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center,
Date: [2003] This title can be found in 1 Iowa libraries.
Experimental investigation of water droplet impingement on airfoils, finite wings, and an S-duct engine inletFormat: [microform] /
Publisher: Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center ;
Date: [2002] This title can be found in 1 Iowa libraries.
Robust airfoil optimization to achieve consistent drag reduction over a mach rangeFormat: [microform] /
Author: Li, Wu.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ;
Date: [2001] This title can be found in 1 Iowa libraries.
Aerodynamic shape optimization of two-dimensional airfoils under uncertain conditionsFormat: [microform] /
Author: Huyse, Luc.
Publisher: Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ;
Date: [2001] This title can be found in 1 Iowa libraries.
ICEG2D (v2.0) an integrated software package for automated prediction of flow fields for single-element airfoils with ice accretion /Format: [microform] :
Author: Thompson, David
Publisher: [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ;
Date: [2001]. This title can be found in 1 Iowa libraries.
Free-form airfoil shape optimization under uncertainty using maximum expected value and second-order second-moment strategiesFormat: [microform] /
Author: Huyse, Luc.
Publisher: Hampton, VA : ICASE, NASA Langley Research Center ;
Date: [2001] This title can be found in 1 Iowa libraries.
Ice accretions and icing effects for modern airfoilsFormat: [microform] /
Author: Addy, Harold E.
Publisher: [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ;
Date: 2000] This title can be found in 1 Iowa libraries.
Implementation of advanced two equation turbulence models in the USM3D unstructured flow solverFormat: [microform] /
Author: Wang, Qunzhen.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ;
Date: [2000] This title can be found in 1 Iowa libraries.
Closed-loop separation control using oscillatory flow excitationFormat: [microform] /
Publisher: Hampton, Va. : ICASE, National Aeronautics and Science Administration, Langley Research Center ;
Date: [2000] This title can be found in 1 Iowa libraries.
Unsteady cascade aerodynamic response using a multiphysics simulation codeFormat: [microform] /
Author: Lawrence, C.
Publisher: Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center ;
Date: [2000] This title can be found in 1 Iowa libraries.
SmaggIce user guide SmaggIce version 1.0 /Format: [microform] :
Author: Baez, Marivell.
Publisher: Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center ;
Date: 2000] This title can be found in 2 Iowa libraries.
The paths of soaring flight /Author: Irving, Frank.
Publisher: River Edge, NJ : Distributed by World Scientific Pub., Singapore ; River Edge, NJ : Distributed by World Scientific Pub.,
Date: c1999. This title can be found in 2 Iowa libraries.
SiC/SiC leading edge turbine airfoil tested under simulated gas turbine conditionsFormat: [microform] /
Author: Robinson, R. Craig.
Publisher: [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ;
Date: [1999] This title can be found in 2 Iowa libraries.
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