Effect of Cavity Width on the Unsteady Pressure in a Low-Mach-Number Cavity

AIAA Journal ◽  
2008 ◽  
Vol 46 (7) ◽  
pp. 1878-1880 ◽  
Author(s):  
Ke Zhang ◽  
Ahmed M. Naguib
Keyword(s):  
Mach Number ◽  
Low Mach Number ◽  
Unsteady Pressure ◽  
Cavity Width

Aerodynamic and Aeroelastic Characteristics of Oscillating Loaded Cascades at Low Mach Number—Part I: Pressure Distribution, Forces, and Moments

1980 ◽  
Vol 102 (2) ◽  
pp. 344-351 ◽  
Author(s):  
H. Atassi ◽  
T. J. Akai
Keyword(s):  
Mach Number ◽  
Pressure Distribution ◽  
Velocity Gradient ◽  
Degrees Of Freedom ◽  
Incompressible Flows ◽  
Complete Theory ◽  
Mean Velocity ◽  
Two Degrees Of Freedom ◽  
Low Mach Number ◽  
Unsteady Pressure

A complete theory is developed in Part I of these two papers for the analysis of oscillating airfoils in cascade in uniform incompressible flows. The theory fully accounts for the geometry of the airfoils and cascade parameters. It is shown that the strong mean velocity gradient near the leading edges of the airfoils significantly affects the unsteady pressure, forces and moments acting upon the airfoils. In Part II the aeroelastic characteristics of a loaded cascade are investigated for one and two degrees of freedom oscillations.

scholarly journals Low Mach number fluctuating hydrodynamics for electrolytes

2016 ◽  
Vol 1 (7) ◽  
Author(s):  
Jean-Philippe Péraud ◽  
Andy Nonaka ◽  
Anuj Chaudhri ◽  
John B. Bell ◽  
Aleksandar Donev ◽  
...  
Keyword(s):  
Mach Number ◽  
Fluctuating Hydrodynamics ◽  
Low Mach Number

scholarly journals An interface capturing method for liquid-gas flows at low-Mach number

2021 ◽  
Vol 216 ◽  
pp. 104789
Author(s):  
Federico Dalla Barba ◽  
Nicoló Scapin ◽  
Andreas D. Demou ◽  
Marco E. Rosti ◽  
Francesco Picano ◽  
...  
Keyword(s):  
Mach Number ◽  
Gas Flows ◽  
Low Mach Number ◽  
Interface Capturing
Sign in / Sign up

Export Citation Format

Share Document