- Additional Authors
- Description
- 1 online resource (19 pages) : color illustrations.
- Series Statement
- NASA/TM ; 2014-218494
- Uniform Title
- NASA technical memorandum ; 2014-218494.
- Subjects
- Note
- Title from title screen (viewed Aug. 7, 2015).
- "November 2014."
- "Prepared for the 50th Joint Propulsion Conference cosponsored by AIAA, ASME, SAE, and ASEE, Cleveland, Ohio, July 28-30, 2014."
- Bibliography (note)
- Includes bibliographical references (page 19).
- Funding (note)
- Sponsored by the Fundamental Aeronautics Program at the NASA Glenn Research Center
- Call Number
- GPO Internet NAS 1.15:2014-218494
- OCLC
- marcive916511610
- Author
Ibrahim, Mounir B., author.
- Title
Computational investigation of novel tip leakage mitigation methods for high pressure turbine blades / Mounir Ibrahim and Abhinav Gupta, Vikram Shyam.
- Publisher
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, November 2014.
- Type of Content
text
- Type of Medium
computer
- Type of Carrier
online resource
- Series
NASA/TM ; 2014-218494
NASA technical memorandum ; 2014-218494.
- Bibliography
Includes bibliographical references (page 19).
- Funding
Sponsored by the Fundamental Aeronautics Program at the NASA Glenn Research Center WBS 473452.02.03.05.04.02.01
E-18962
- Connect to:
- Added Author
Gupta, Abhinav, author.
Shyam, Vikram, author.
NASA Glenn Research Center, issuing body.
Fundamental Aeronautics Program (U.S.), sponsoring body.
- Gpo Item No.
0830-D (online)
- Sudoc No.
NAS 1.15:2014-218494