Research Catalog
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Displaying 1-4 of 4 results
Flow visualization study of the effect of injection hole geometry on an inclined jet in crossflow [microform] / Frederick F. Simon and Michael L. Ciancone.
- Text
- [Washington, D.C.] : National Aeronautics and Space Administration, [1985]
- 1985
Long hole film cooling dataset for CFD development. Part 1. Infrared thermography and thermocouple surveys / Vikram Shyam [and five others].
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, 2013.
- 2013
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo51647Computational investigation of novel tip leakage mitigation methods for high pressure turbine blades / Mounir Ibrahim and Abhinav Gupta, Vikram Shyam.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, November 2014.
- 2014-11
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo57875Design evaluation using finite element analysis of cooled silicon nitride plates for a turbine blade application / Ali Abdul-Aziz, George Y. Baaklini, Ramakrishna T. Bhatt.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, June 2001.
- 2001-6
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/LPS23306
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