Compressible Flows: Supersonic, Hypersonic and General (3:55pm - 4:40pm CST)

Presentations

• Stepped aerospike for enhanced drag reduction using multiple intermediate shocks.

  POSTER

  Authors

  • Ankit Kumar

    • Indian Institute of Technology, Kharagpur

  • Swapnil Majumder

    • Indian Institute of Technology, Kharagpur

  • Sandeep Saha

    • Assistant Professor
    • Indian Institute of Technology Kharagpur
    • Indian Institute of Technology, Kharagpur

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• Dynamics of compound, compressible flow contractions

  POSTER

  Authors

  • Jean-Pierre Hickey

    • University of Waterloo
    • Mechanical and Mechatronics Engineering, University of Waterloo

  • Hamid Daryan

    • University of Waterloo

  • Khaled Younes

    • University of Waterloo

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• Experimental analysis of diffuser terminal shock motion and associated acoustics in vacuum objective supersonic air ejectors

  POSTER

  Authors

  • Jesse Morales

    • University of British Columbia Okanagan

  • Deepanshi Sisodiya

    • University of British Columbia Okanagan

  • Joshua Brinkerhoff

    • University of British Columbia Okanagan
    • University of British Columbia
    • University of British Columbia - Okanagan campus
    • The University of British Columbia - Okanagan Campus

  • Sina Kheirkhah

    • University of British Columbia
    • University of British Columbia Okanagan
    • School of Engineering, University of British Columbia, Kelowna, Canada, V1V 1V7

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• Shock Wave Oscillation at Cylindrical Cavity on Wedge Surface in Mach-7 Hypersonic Flow.

  POSTER

  Authors

  • Yasumasa Watanabe

    • The University of Tokyo

  • Aleksandar Jemcov

    • University of Notre Dame

  • Hirotaka Sakaue

    • University of Notre Dame

  • Joseph Gonzales

    • University of Notre Dame

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• Self-sustained Shock Oscillations over Axisymmetric Bodies in Hypersonic Flow

  POSTER

  Authors

  • Vaisakh Sasidharan

    • Indian Institute of Science

  • Subrahmanyam Duvvuri

    • Indian Institute of Science

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• Reynolds number dependency on Lagrangian Coherent Structures (LCS) over supersonic turbulent boundary layers

  POSTER

  Authors

  • German Saltar Rivera

    • HPCVLab, Dept. of Mechanical Eng., U. of Puerto Rico-Mayaguez

  • Guillermo Araya

    • University of Puerto Rico at Mayaguez
    • HPCVLab, U. of Puerto Rico-Mayaguez
    • HPCVLab, Dept. of Mechanical Eng., U. of Puerto Rico-Mayaguez

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• Influences of forebody size on supersonic retropropulsion flowfield dynamics

  POSTER

  Authors

  • Owen Williams

    • University of Washington

  • Maxine Tan

    • University of Washington

  • Xiuqi Yang

    • University of Washington

  • Brenton Ho

    • University of Washington

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• Input/output Analysis of Hypersonic Boundary Layers using the One-Way Navier-Stokes (OWNS) Equations

  POSTER

  Authors

  • Omar Kamal

    • Caltech

  • Georgios Rigas

    • Imperial College London

  • Matthew Lakebrink

    • The Boeing Company

  • Tim Colonius

    • Caltech
    • California Institute of Technology

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• Delay of high-speed boundary-layer transition by isolated roughness

  POSTER

  Authors

  • Reza Jahanbakhshi

    • Florida Inst of Tech

  • Tamer Zaki

    • Johns Hopkins University
    • Department of Mechanical Engineering, John Hopkins University,USA

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• Numerical subgrid-scale modeling of supersonic spatially-developing turbulent boundary layers

  POSTER

  Authors

  • Guillermo Araya

    • University of Puerto Rico at Mayaguez
    • HPCVLab, U. of Puerto Rico-Mayaguez
    • HPCVLab, Dept. of Mechanical Eng., U. of Puerto Rico-Mayaguez

  • Andres Tejada-Martinez

    • Univ of South Florida
    • University of South Florida, Department of Civil and Environmental Engineering
    • U. of South Florida

  • Kenneth Jansen

    • U. of Colorado-Boulder

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