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.
Transonic airfoil design code
NASA Tech Briefs ; 5 , 1
1980-08-01
Miscellaneous
No indication
English
AIAA | 1971
|Transonic airfoil analysis and design
NTRS | 1980
|NTRS | 1984
|Transonic airfoil design using Cartesian coordinates
TIBKAT | 1975
|