Numerical Aerodynamics at DLR

نویسندگان
چکیده

برای دانلود باید عضویت طلایی داشته باشید

برای دانلود متن کامل این مقاله و بیش از 32 میلیون مقاله دیگر ابتدا ثبت نام کنید

اگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید

منابع مشابه

Concurrent Launcher Engineering at Dlr

The SART (Space Launcher Systems Analysis) group of the German Aerospace Center DLR has the task of examining all types of future space launch systems and the thereof required engines by means of modern, computer-aided methods. One of the fundamental aims is to reduce the cost of access to space through the identification of eligible technology. Activities range from stand-alone preliminary stu...

متن کامل

Aerodynamics an aerofoil in transonic ground effect : numerical study at full - scale Reynolds num rs

The potential positive effects of ground proximity on the aerodynamic performance of a \Ving or aerofoil have long been established, but at transonic speeds the fonnation of shock waves betvveen the body and the ground plane would have significant consequences. A numerical study of the aerodynamics of an lu\E2822 aerofoil section in ground eiiect flight was conducted at freestream Mach numbers ...

متن کامل

Numerical Simulation of Kinetic Effects in Low-density Hypersonic Aerodynamics

The Direct Simulation Monte-Carlo technique (DSMC) is used for numerical analysis of rarefied-gas hypersonic flows near a blunt plate, wedge, two side-by-side plates and cylinders, sphere, torus, and rotating cylinder. Important kinetic effects that are specific for the transition flow regime have been found: nonmonotonic lift of plates, strong repulsive force between side-by-side plates and cy...

متن کامل

Numerical Modelling of Corona Discharges and Their Interaction with Aerodynamics

In the frame of the internal project PUMA (Plasma Used to Master Aerodynamic), ONERA is conducting fundamental studies in order to determine the limits within which air discharge plasmas are able to interact with aerodynamical phenomena. This paper focuses on the physical and numerical modeling of corona discharges and their interaction with aerodynamics. Using a simple plasma kinetic scheme, i...

متن کامل

Numerical and Experimental Investigation of Helicopter Fuselage Aerodynamics

The aerodynamic characteristics of an isolated MRH 90 helicopter fuselage have been investigated using Computational Fluid Dynamics (CFD). Simulations utilised an unstructured tetrahedral grid and both the k-ε and k-ω SST turbulence models were investigated. Standard ‘law of the wall’ wall functions were incorporated, along with a segregated finite volume solver. A wind tunnel testing program w...

متن کامل

ذخیره در منابع من


  با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید

ژورنال

عنوان ژورنال: Chinese Journal of Aeronautics

سال: 2006

ISSN: 1000-9361

DOI: 10.1016/s1000-9361(11)60293-8