NASA NTRS · 19700068467
Flow with M/infinity/equals 1 past thin airfoils
Abstract
Pressure distribution on thin nonlifting airfoils in steady two dimensional flow with freestream Mach number at or near unity
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Spreiter, J. R., Stahara, S. S.. 1970-10-01. Flow with M/infinity/equals 1 past thin airfoils. https://ntrs.nasa.gov/citations/19700068467
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