Compressible Flows: General
ORAL · J10 · ID: 678120
Presentations
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On the Integrability of Subsonic Compressible Potential Flow Around Cylinders
ORAL
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Presenters
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Roy S Baty
Los Alamos Natl Lab
Authors
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Roy S Baty
Los Alamos Natl Lab
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Scott D Ramsey
Los Alamos Natl Lab
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On the Integrability of Subsonic Compressible Potential Flow Around Bodies of Revolution
ORAL
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Presenters
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Scott D Ramsey
Los Alamos Natl Lab
Authors
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Scott D Ramsey
Los Alamos Natl Lab
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Roy S Baty
Los Alamos Natl Lab
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Application of the Janzen-Rayleigh Method to Obstructed Flow
ORAL
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Presenters
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Tyler Remedes
Los Alamos National Laboratory
Authors
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Tyler Remedes
Los Alamos National Laboratory
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Scott D Ramsey
Los Alamos Natl Lab
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Roy S Baty
Los Alamos Natl Lab
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Flow unsteadiness in the near-wake of a supersonic cylinder
ORAL
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Presenters
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Ravi Sankar Vaddi
Indian Institute of Science Bangalore
Authors
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Ravi Sankar Vaddi
Indian Institute of Science Bangalore
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Premika S Thasu
Indian Institute of Science Bangalore
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Subhajit Das
Indian Institute of Science Bangalore
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Subrahmanyam Duvvuri
Indian Institute of Science Bangalore
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Large-eddy simulation of a Mach 6 cylinder wake
ORAL
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Presenters
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Gaurav Kumar
Indian Institute of Science Bangalore
Authors
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Gaurav Kumar
Indian Institute of Science Bangalore
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Subrahmanyam Duvvuri
Indian Institute of Science Bangalore
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Investigation of Mach number effects on flow over a rectangular cylinder around critical geometry at Reynolds number O(10<sup>3</sup>) using a low-density wind tunnel
ORAL
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Presenters
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Satoshi Kimura
Tohoku University
Authors
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Satoshi Kimura
Tohoku University
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Takayuki Nagata
Tohoku University
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Miku Kasai
Tohoku University
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Yuta Ozawa
Tohoku Univ, Tohoku University
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Taku Nonomura
Tohoku Univ, Tohoku University
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TRANSIENT PHENOMENA ASSOCIATED WITH MODE TRANSITION IN STRUT-BASED DUAL-MODE SCRAMJET ENGINES
ORAL
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Publication: Kumar, Rajesh, Saisanthosh G. Iyer, Narne Prudhvi, and Amardip Ghosh. "Mode Transition in a Strut Based Dual-Mode Scramjet Combustor." In AIAA AVIATION 2022 Forum, p. 3863. 2022. https://doi.org/10.2514/6.2022-3863
Presenters
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Rajesh Kumar
INDIAN INSTITUTE OF TECHNOLOGY KHARAGPUR
Authors
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Rajesh Kumar
INDIAN INSTITUTE OF TECHNOLOGY KHARAGPUR
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AMARDIP GHOSH
INDIAN INSTITUTE OF TECHNOLOGY KHARAGPUR
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Leading-edge separation in hypersonic flow
ORAL
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Publication: A full-length manuscript based on the parts of the present abstract is being prepared to be submitted to Experiments in Fluids.
Presenters
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Karthick SK
Technion - Israel Institute of Technology
Authors
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Karthick SK
Technion - Israel Institute of Technology
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Soumya R Nanda
Technion - Israel Institute of Technology
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Jacob Cohen
Technion - Israel Institute of Technology
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Alternative Analytical Solution for Planar Oblique Shock Waves
ORAL
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Presenters
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Steven A Miller
University of Florida
Authors
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Steven A Miller
University of Florida
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Steady, Quasi-One-Dimensional, Internal Compressible Flow with Area Change, Heat Addition, and Friction
ORAL
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Publication: Steady, Quasi-One-Dimensional, Internal Compressible Flow with Area Change, Heat Addition, and Friction. Submitted to Journal of Fluid Mechanics. 2022. Currently under revision.
Presenters
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Andrew A Oliva
University of Notre Dame
Authors
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Andrew A Oliva
University of Notre Dame
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Scott C Morris
University of Notre Dame
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Multi-Scale Modeling of a Shock Tube to Examine Shock-Droplet Interaction
ORAL
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Publication: A Computational Fluid Dynamics Model of Shockwave Initiated Combustion, RW Forehand, MP Kinzel<br>AIAA AVIATION 2022 Forum, 3842, 2022<br>Numerical Modeling of Shockwave Initiated Combustion of a Hydrogen-Oxygen Mixture Within a Shock Tube, RW Forehand, University of Central Florida Thesis, 2021
Presenters
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Reed W Forehand
University of Central Florida
Authors
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Reed W Forehand
University of Central Florida
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Khanh C Nguyen
University of Central Florida
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Sydney Briggs
University of Central Florida
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Nicolas Berube
University of Central Florida
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Caroline J Anderson
University of Central Florida
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Michael P Kinzel
University of Central Florida, university of central florida
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Subith Vasu
University of Central Florida
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Sheryl M Grace
Boston University
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Machine Learning with Supersonic Retropropulsion Wind Tunnel Test Data
ORAL
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Presenters
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David Wu
Stanford University
Authors
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David Wu
Stanford University
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Wai Tong Chung
Stanford University
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Matthias Ihme
Stanford University
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Karl Edquist
NASA Langley Research Center
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