NASA NTRS · 19800000085
Transonic airfoil design code
Abstract
Program aids in design of shockless airfoils, assists development of fuel-conserving, supercritical wings. Algorithm calculates approximate airfoil shape given prescribed pressure distribution. This allows design of families of transonic airfoils for use in aircraft wings or turbine and compressor blades. Program is written in FORTRAN IV for batch execution on CDC-6000.
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Bauer, F., Garabedian, P., Korn, D.. 1980-08-01. Transonic airfoil design code. https://ntrs.nasa.gov/citations/19800000085
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