Navier-Stokes and Euler Computations of the Flow Field Around a Complete Aircraft Lockheed Aeronautical Systems Company, Burbank, CA

Format:

Conference/Event

Author/Creator:

Olling, Charles R., author.

Conference Name:

Aerospace Technology Conference & Exposition (1988-10-03 : Anaheim, California, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1988

Summary:

The flow field around a complete supersonic V/STOL configuration was computed by solving the Euler and thin-layer Navier-Stokes equations with a multizone, finite-volume, explicit Runge-Kutta time-stepping method. The Navier-Stokes equations were solved in specified zones and the Euler equations were solved in the remaining zones. The Baldwin-Lomax turbulence model was applied for the Navier-Stokes computations. A global grid for the complete aircraft configuration was generated with an optimization method and divided into a multizone grid. The computed lift coefficients and pressure on the wing surface were compared with experimental data

Notes:

Vendor supplied data

Publisher Number:

881488

Access Restriction:

Restricted for use by site license