Zobrazeno 1 - 10 of 10 pro vyhledávání: '"Derick Daniel"'
1
Direct Skin Friction Measurements at Mach 10 in a Hypervelocity Wind Tunnel
Autor: Ryan J. Meritt, Daniel R. Lewis, Derick Daniel, Joseph A. Schetz, Eric C. Marineau
Publikováno v: Journal of Spacecraft and Rockets. 54:871-882
This investigation concerns the design, build, and testing of direct-measuring skin friction sensors capable of performing in sustained hypersonic flow and detecting transition. A multistep approac...
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::7f9e4dbefff207023e3dd218148b009f
https://doi.org/10.2514/1.a33657
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6
A Survey of Solver-Related Geometry and Meshing Issues
Autor: Jared Gudenkauf, David Hine, Chris Sideroff, Derick Daniel, James S. Masters
Publikováno v: 46th AIAA Fluid Dynamics Conference.
There is a concern in the computational fluid dynamics community that mesh generation is a significant bottleneck in the CFD workflow. This is one of several papers that will help set the stage for a moderated panel discussion addressing this issue.
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::be438a094a266b5cec34c96731956a1d
https://doi.org/10.2514/6.2016-3487
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7
Hypersonic Boundary Layer Transition Experiments in Hypervelocity Ballistic Range G
Autor: Taylor A. Swanson, Derick Daniel
Publikováno v: 54th AIAA Aerospace Sciences Meeting.
Hypersonic boundary layer transition impacts vehicles through increased heat transfer and drag, alters a vehicle’s flight path, and is of great concern for hypersonic vehicles. However, it is difficult to predict real world full scale performance w
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::7c810c5ed072357931b22db3037bc77c
https://doi.org/10.2514/6.2016-2118
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8
Numerical Investigations of Flow Separation on the AVT-183 53 Degree Swept Diamond Wing Configuration
Autor: Donald J. Malloy, Derick Daniel, Daniel A. Reasor, Craig C. Morris
Publikováno v: 53rd AIAA Aerospace Sciences Meeting.
This investigation comparing wind tunnel results and pretest and posttest CFD predictions was undertaken as part of the NATO AVT-183 task group, which was established for the purpose of assessing the reliable prediction of separation onset for flows
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::ab1714ea3a3cfcd769c646ef67459c07
https://doi.org/10.2514/6.2015-0066
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9
Applicability of Hybrid RANS/LES Models in Predicting Separation Onset of the AVT-183 Diamond Wing
Autor: Derick Daniel, Donald J. Malloy, Daniel A. Reasor
Publikováno v: 53rd AIAA Aerospace Sciences Meeting.
This effort contributes to the understanding of hybrid RANS/LES turbulence model behavior for prediction of separation onset via an investigation of the accuracy and predictions of the SARC-DDES variant. The focus is not to interrogate the underlying
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::17798281017cd0064e80ed0bee02f1f6
https://doi.org/10.2514/6.2015-0287
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10
A General Simulation of an Air Ejector Diffuser System
Autor: Derick Daniel
Publikováno v: 28th Aerodynamic Measurement Technology, Ground Testing, and Flight Testing Conference.
A computer model of a blow-down free-jet hypersonic propulsion test facility exists to validate facility control systems as well as predict problems with facility operation. One weakness in this computer model is the modeling of an air ejector diffus
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::ad04f7c2a219d91cdfbbcc41eabbea62
https://doi.org/10.2514/6.2012-3292
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