The codes were developed by Dr. Rodrick V. Chima at NASA Glenn Research Center. They have been validated and have been heavily used at NASA Glenn and in U.S. industries and universities for a wide variety of problems including analysis of the Space Shuttle main engine turbopumps and the design of transonic fan blades.
Namelist input is used, and some printed output is generated.
The codes are generally available to universities or companies within the United States . For technical information, please consult the references. To obtain any of the codes, please contact me directly at the address below. A formal letter of request including information on your intended applications will be required. University students should request the codes through their faculty advisor.