Research Catalog

Title

Experimental and computational investigation of the tip clearance flow in a transonic axial compressor rotor [microform] / Kenneth L. Suder and Mark L. Celestina.

Author

Suder, Kenneth L.

Publication

[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]

Details

Additional Authors

• Celestina, Mark L.
• United States. National Aeronautics and Space Administration.

Description

1 v.

Series Statement

NASA technical memorandum ; 106711

Subject

• Airspeed
• Applications programs (Computers)
• Blade tips
• Blade-vortex interaction
• Compressor rotors
• Laser anemometers
• Shock wave interaction
• Tip speed
• Transonic compressors
• Turbo compressors
• Vortices
• Wall flow

Note

• Distributed to depository libraries in microfiche.
• Shipping list no.: 96-0021-M.

Reproduction (note)

• Microfiche.

Call Number

READEX Microfiche NAS 1.15:106711

OCLC

marcive34041388

Author

Suder, Kenneth L.

Title

Experimental and computational investigation of the tip clearance flow in a transonic axial compressor rotor [microform] / Kenneth L. Suder and Mark L. Celestina.

Imprint

[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]

Series

NASA technical memorandum ; 106711

Reproduction

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 1 microfiche.

Added Author

Celestina, Mark L.

United States. National Aeronautics and Space Administration.

Gpo Item No.

0830-D (MF)

Sudoc No.

NAS 1.15:106711

Research Call Number

READEX Microfiche NAS 1.15:106711