by Iowa State University., Engineering Research Institute, National Aeronautics and Space Administration, National Technical Information Service, distributor in [Ames, Iowa], [Washington, DC, Springfield, Va .
Written in English
|Statement||by D. Lee, R.H. Pletcher|
|Series||NASA contractor report -- NASA CR-179900|
|Contributions||Pletcher, Richard H, United States. National Aeronautics and Space Administration|
|The Physical Object|
Get this from a library! Application of viscous-inviscid interaction methods to transonic turbulent flows. [D Lee; Richard H Pletcher; United States. National Aeronautics and Space Administration.]. For aerofoils a calculation, which involves the coupling of the external inviscid flow with the viscous flow in the boundary layer and the wake, still provides a worthwhile alternative to the solution of the ‘time-averaged’ Navier-Stokes equations. Classical viscous-inviscid interaction methods which can be extended to include flows with separations and significant pressure Cited by: 2. Meanwhile separation on a smooth surface is accompanied by a more traditional viscous-inviscid separation. However, unlike in subsonic or supersonic flow, the boundary layer immediately upstream of the interaction region has a preseparated form. This results in a hysteresis character of the flow behaviour in the interaction by: 1. Subsequently, Buldakov & Ruban () used the analytical methods along with computations to study inviscid transonic flow in the vicinity of the sonic point on a .
Numerical simulations of incompressible aerodynamic flows using viscous/inviscid interaction procedures Article in Computer Methods in Applied Mechanics and . Theory of laminar viscous-inviscid interactions in supersonic flow. Transonic turbulent viscous-inviscid interaction over airfoils. T. TAI; Supersonic separated and reattaching laminar flows- i - general theory and application to adiabatic boundary layer Cited by: Viscous - Inviscid Interaction Methods for Flutter Calculations Widjaja Kresna Sekar Vollständiger Abdruck der von der Fakultät für Maschinenwesen der Technischen Universität München zur Erlangung des akademischen Grades eines Doktor-Ingenieurs genehmigten Dissertation. Vorsitzender: Univ. -Prof. Dr. –Ing. habil. Nikolaus A. Adams. Viscous–inviscid interactions in transonic flows through slender nozzles - Volume - A. KLUWICK, G. MEYER. you will be asked to authorise Cambridge Core to connect with your account. Find out more about sending content to Dropbox. Viscous–inviscid interactions in transonic flows through slender by: 8.
ISBN: OCLC Number: Notes: "The Second Symposium on Numerical and Physical Aspects of Aerodynamic Flows was held at California State University, Long Beach from 17 to 20 January "--Page vii. Viscous-Inviscid Analysis of Transonic and Low Reynolds Number Airfoils Mark Drela* and Michael B. Gilest Massachusetts Institute of Technology, Cambridge, Massachusetts A method of accurately calculating transonic and low Reynolds number airfoil flows, implemented in the viscous-inviscid design/analysis code ISES, is presented. VISCOUS-INVISCID INTERACTION IN A TRANSONIC FLOW CAUSED BY A DISCONTINUITY IN WALL CURVATURE A thesis submitted to the University of Manchester for the degree of Doctor of Philosophy in the Faculty of Engineering and Physical Sciences Dmitry Yumashev School of Mathematics. () Analysis of viscous-inviscid interaction in transonic internal flows. AIAA Journal , () Interaction of a turbulent boundary layer with Cited by: