Publication Date:
2006-02-14
Description:
The effort to develop classical methods to compute wall interference at transonic speeds is outlined. The two-dimensional theory and three-dimensional development are discussed. Also, some numerical application of the two-dimensional work are indicated. The basic advantages of the asymptotic theory are noted.
Keywords:
AERODYNAMICS
Type:
NASA. Langley Research Center Wind Tunnel Wall Interference Assessment and Correction, 1983; p 193-203
Format:
text