NASA NTRS · 19770023142
Study of design and analysis methods for transonic flow
Abstract
An airfoil design program and a boundary layer analysis were developed. Boundary conditions were derived for ventilated transonic wind tunnels and performing transonic windtunnel wall calculations. A computational procedure for rotational transonic flow in engine inlet throats was formulated. Results and conclusions are summarized.
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Murman, E. M.. 1977-07-01. Study of design and analysis methods for transonic flow. https://ntrs.nasa.gov/citations/19770023142
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