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Analysis Of A High Speed Civil Transport Configuration At Subsonic Flow Conditions Using A Navier Stokes Solver
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Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722082031 Total Pages :40 pages Book Rating :4.0/5 (82 download)
Book Synopsis Analysis of a High Speed Civil Transport Configuration at Subsonic Flow Conditions Using a Navier-Stokes Solver by : National Aeronautics and Space Administration (NASA)
Download or read book Analysis of a High Speed Civil Transport Configuration at Subsonic Flow Conditions Using a Navier-Stokes Solver written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-06-30 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt: Computations of three dimensional vortical flows over a generic High Speed Civil Transport (HSCT) configuration with an aspect ratio of 3.04 are performed using a thin-layer Navier-Stokes solver. The HSCT cruise configuration is modeled without leading or trailing edge flap deflections and without engine nacelles. The flow conditions, which correspond to tests done in the NASA Langley 8-Foot Transonic Pressure Tunnel (TPT), are a subsonic Mach number of 0.3 and Reynolds number of 4.4 million for a range-of-attack (-.23 deg to 17.78 deg). The effects of the farfield boundary location with respect to the body are investigated. The boundary layer is assumed turbulent and simulated using an algebraic turbulence model. The key features of the vortices and their interactions are captured. Grid distribution in the vortex regions is critical for predicting the correct induced lift. Computed forces and surface pressures compare reasonably well with the experimental TPT data. Lessard, Victor R. Unspecified Center NAS1-18585; RTOP 537-03-22-02...
Book Synopsis Analysis of a High Speed Civil Transport Configuration at Subsonic Flow Conditions Using a Navier-Stokes Solver by : Victor R. Lessard
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