A Linearized Model for Compressible Flow past a Rotating Obstacle: Analysis via Modified Bochner–Riesz Multipliers

2015 ◽  
Vol 34 (3) ◽  
pp. 285-308
Author(s):  
Reinhard Farwig ◽  
Milan Pokorný
Keyword(s):  
Compressible Flow ◽  
Flow Past ◽  
Rotating Obstacle ◽  
Linearized Model ◽  
Obstacle Analysis

Stability of the Low Reynolds Number Compressible Flow Past a NACA0012 Airfoil

AIAA Journal ◽  
2021 ◽  
pp. 1-15
Author(s):  
Laura Victoria Rolandi ◽  
Thierry Jardin ◽  
Jérôme Fontane ◽  
Jérémie Gressier ◽  
Laurent Joly
Keyword(s):  
Reynolds Number ◽  
Compressible Flow ◽  
Low Reynolds Number ◽  
Naca0012 Airfoil ◽  
Flow Past ◽  
Low Reynolds

Boundary-Layer Characteristics of Compressible Flow past a Heated Cylinder with Viscous Dissipation

2019 ◽  
Vol 33 (1) ◽  
pp. 10-22 ◽  
Author(s):  
Nepal C. Roy ◽  
T. Rahman ◽  
M. A. Hossain ◽  
Rama Subba Reddy Gorla
Keyword(s):  
Boundary Layer ◽  
Compressible Flow ◽  
Viscous Dissipation ◽  
Heated Cylinder ◽  
Flow Past

Mathematical Problems in Transonic Flow

1986 ◽  
Vol 29 (2) ◽  
pp. 129-139 ◽  
Author(s):  
Cathleen Synge Morawetz
Keyword(s):  
Compressible Flow ◽  
Transonic Flow ◽  
Supersonic Flight ◽  
Flow Past ◽  
Mathematical Problems

AbstractWe present an outline of the problem of irrotational compressible flow past an airfoil at speeds that lie somewhere between those of the supersonic flight of the Concorde and the subsonic flight of commercial airlines. The problem is simplified and the important role of modifying the equations with physics terms is examined.

Effect of Mach number on the compressible flow past a wavy-axis cylinder

2020 ◽  
Vol 104 ◽  
pp. 105943
Author(s):  
Chang-Yue Xu ◽  
Bin Hou ◽  
Zhe Wang ◽  
Yan-Tai Zhang ◽  
Jian-Hong Sun
Keyword(s):  
Mach Number ◽  
Compressible Flow ◽  
Flow Past ◽  
Axis Cylinder

A hybrid method for transonic flow past multi-element aerofoils

1986 ◽  
Vol 170 ◽  
pp. 253-264 ◽  
Author(s):  
M. G. Hill ◽  
N. Riley
Keyword(s):  
Finite Difference ◽  
Finite Difference Method ◽  
Compressible Flow ◽  
Hybrid Method ◽  
Difference Method ◽  
Transonic Flow ◽  
Potential Flow ◽  
Supercritical Flow ◽  
Subcritical Flow ◽  
Flow Past

A method for calculating transonic potential flow past a multi-element aerofoil configuration is presented. The method is a hybrid method that is based upon a compressible-flow panel method, valid for subcritical flow, and a finite-difference method that is suitable for supercritical flow calculations. The effectiveness of the proposed method is demonstrated, first by application to a single aerofoil and then to a three-element aerofoil.

Slow Compressible Flow past a Circular Cylinder

1968 ◽  
Vol 11 (8) ◽  
pp. 1636 ◽  
Author(s):  
P. F. Hodnett
Keyword(s):  
Circular Cylinder ◽  
Compressible Flow ◽  
Flow Past
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