Transonic separated solutions for an augmentor-wingThe viscous transonic flow about a multielement airfoil (augmentor-wing) is simulated by coupling full-potential and direct/inverse differential boundary-layer algorithms. Solutions have been obtained for a variety of conditions and are in fair agreement with available experimental data. Typical results from this transonic augmentor-wing code (TAUG-V) require approximately three minutes of CRAY-XMP CPU time. Since this viscous transonic code accounts for most of the important flow physics, yet is still economical, it is a practical tool for the design aerodynamicist.
Document ID
19860026321
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Flores, J. (NASA Ames Research Center Moffett Field, CA, United States)
Van Dalsem, W. R. (NASA Ames Research Center Moffett Field, CA, United States)