Numerical Anaylsis of Compressible Flow Around Three-Dimensional Fin-Body Combination Dept. of Aeronautical Eng., Seoul National Univ

Format:

Conference/Event

Author/Creator:

Rho, Ohyun, author.

Conference Name:

Aerospace Technology Conference & Exposition (1990-10-01 : Long Beach, California, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1990

Summary:

The existing two-dimensional Euler code is extended to the three-dimensional flow problem in which the transonic flow around the double fin-body combinations was analysed. Ni's two-dimensional formulas are extended to the three-dimensional case and applied to the supersonic flow calculation over the double fin-body combinations.The numerical results have proved to be very accurate in predicting the pressure distribution and capturing the shock. The code extended to the three-dimensional flow analysis in the paper can be consequently used to estimate the aerodynamic characteristics of the complicated body

Notes:

Vendor supplied data

Publisher Number:

901812

Access Restriction:

Restricted for use by site license