CFL3D contribution to the AIAA Supersonic Shock Boundary Layer Interaction Workshop /
Saved in:
Author / Creator: | Rumsey, C. L. (Christopher Lockwood), 1961- |
---|---|
Imprint: | Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2010] |
Description: | 1 online resource (29p.) : col. ill. |
Language: | English |
Series: | NASA/TM ; 2010-216858 NASA technical memorandum ; 216858. |
Subject: | Shock layers. Supersonic boundary layers. Turbulence models. Mathematical models. Computational fluid dynamics. Computational fluid dynamics. Mathematical models. |
Format: | E-Resource U.S. Federal Government Document Book |
URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/8507894 |
Varying Form of Title: | Computational Fluids Laboratory 3-Dimensional contribution to the AIAA Supersonic Shock Boundary Layer Interaction Workshop |
---|---|
Other authors / contributors: | Langley Research Center. AIAA Supersonic Shock Boundary Layer Interaction Workshop (2010 : Orlando, Fla.) |
Notes: | Title from title screen (viewed on Sept. 8, 2011). "October 2010." Includes bibliographical references (p. 7). 561581.02.08.07.20.14 |
GPO item no.: | 0830-D (online) |
Govt.docs classification: | NAS 1.15:2010-216858 |
Similar Items
-
Wind-US code contributions to the first AIAA Shock Boundary Layer Interaction Prediction Workshop /
by: Georgiadis, Nicholas J.
Published: (2013) -
Summary of EASM turbulence models in CFL3D with validation test cases /
by: Rumsey, C. L. (Christopher Lockwood), 1961-
Published: (2003) -
Summary of EASM turbulence models in CFL3D with validation test cases /
by: Rumsey, C. L. (Christopher Lockwood), 1961-
Published: (2003) -
Assessment of computational fluid dynamics (CFD) models for shock boundary-layer interaction /
Published: (2011) -
CFD validation experiment of a Mach 2.5 axisymmetric shock-wave/boundary-layer interaction /
by: Davis, David O.
Published: (2015)