Computational investigation of novel tip leakage mitigation methods for high pressure turbine blades /

Bibliographic Details

Main Authors:	Ibrahim, Mounir B. (Author), Gupta, Abhinav (Author), Shyam, Vikram (Author)
Corporate Author:	Fundamental Aeronautics Program (U.S.) (sponsoring body.)
Format:	Government Document eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, November 2014.
Series:	NASA technical memorandum ; 2014-218494.
Subjects:	Computational fluid dynamics. Turbine blades. Rotor blades (turbomachinery) Hole distribution (mechanics) Hole geometry (mechanics)
Online Access:	https://purl.fdlp.gov/GPO/gpo57875 http://purl.fdlp.gov/GPO/gpo57875