Research Catalog

Title

Comparison of various supersonic turbine tip designs to minimize aerodynamic loss and tip heating / Vikram Shyam, Ali Ameri.

Author

Shyam, Vikram.

Publication

Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]

Details

Additional Authors

• Ameri, Ali.
• NASA Glenn Research Center.
• ASME Turbo Expo (2011 : Vancouver, B.C.)

Description

1 online resource (8 pages) : illustrations (some color).

Series Statement

NASA/TM ; 2012-217607

Uniform Title

NASA technical memorandum ; 2012-217607.

Subject

• Computational fluid dynamics
• Supersonic turbines
• Blade tips
• Supersonic flow
• Rotor aerodynamics
• Axial flow turbines
• Supersonic heat transfer
• Contours

Note

• Title from title screen (viewed on Dec. 3, 2012).
• "July 2012."
• "Prepared for the TURBO EXPO 2011 sponsored by the American Society of Mechanical Engineers (ASME) Vancouver, British Columbia, June 6-10, 2011."
• "GT2011-46390."

Bibliography (note)

• Includes bibliographical references (page 8).

Funding (note)

• Sponsored by National Aeronautics and Space Administration

Call Number

GPO Internet NAS 1.15:2012-217607

OCLC

marcive820022602

Author

Shyam, Vikram.

Title

Comparison of various supersonic turbine tip designs to minimize aerodynamic loss and tip heating / Vikram Shyam, Ali Ameri.

Publisher

Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]

Type of Content

text

Type of Medium

computer

Type of Carrier

online resource

Series

NASA/TM ; 2012-217607

NASA technical memorandum ; 2012-217607.

Bibliography

Includes bibliographical references (page 8).

Funding

Sponsored by National Aeronautics and Space Administration WBS 561581.02.08.03.21.14.03

E-18188

Connect to:

https://purl.fdlp.gov/GPO/gpo31866

Added Author

Ameri, Ali.

ASME Turbo Expo (2011 : Vancouver, B.C.)

NASA Glenn Research Center.

Gpo Item No.

0830-D (online)

Sudoc No.

NAS 1.15:2012-217607