Sciences & Technologie
Volume 2, Numéro 1, Pages 19-23
2017-06-30
Authors : Nahoui Azzedine . Bahi Lakhdar .
Reduce energy consumption of airplanes, or enhance the aerodynamic performance of compressors and turbines by reducing drag, or increasing lift is a major challenge for many institutions specializing in aerodynamics [1, 2]. One way to achievethis, isconsidered the study of compressible potential flow compared to incompressible potential flow [3], Outside the boundary layer, to study the effects of compressibility and the control parameters. And the pressure coefficient and lift distributions around the NACA 0012 profile, NACA 0015 and NACA 0018 were studied and presented in terms of the Mach number, angle of attack and the relative thickness of the profiles.
compressibilité, coefficient de pression, coefficient de portance
Nahoui Azzedine
.
Bahi Lakhdar
.
pages 09-14.
Nahoui Azzedine
.
Bahi Lakhdar
.
pages 9-14.
Hallouz Faiza
.
Meddi Mohamed
.
Mahé Gil
.
pages 37-47.
Randolph Brian
.
Cisarik Patricia M.
.
pages 130-138.
بوعلي لخضر
.
نمرود بشير
.
ناصر محمد
.
ص 426-445.