Research Catalog

Title

Experimental investigation of wing installation effects on a two-dimensional mixer/ejector nozzle for supersonic transport aircraft [microform] / David J. Anderson, Heather H. Lambert, and Masashi Mizukami.

Author

Anderson, David J.

Publication

[Washington, D.C.] : NASA ; [Springfield, Va. : National Technical Information Service, distributor, 1992]

Details

Additional Authors

• Lambert, Heather H.
• Mizukami, Masashi.
• United States. National Aeronautics and Space Administration.

Description

1 v.

Series Statement

NASA technical memorandum ; 105713

Subject

• Acoustic properties
• Ejectors
• Engine airframe integration
• Exhaust nozzles
• Flow distribution
• Inlet flow
• Noise reduction
• Nozzle flow
• Supersonic transports
• Wind tunnel tests
• Wings

Note

• Distributed to depository libraries in microfiche.

Reproduction (note)

• Microfiche.

Call Number

READEX Microfiche NAS 1.15:105713

OCLC

marcive34778135

Author

Anderson, David J.

Title

Experimental investigation of wing installation effects on a two-dimensional mixer/ejector nozzle for supersonic transport aircraft [microform] / David J. Anderson, Heather H. Lambert, and Masashi Mizukami.

Imprint

[Washington, D.C.] : NASA ; [Springfield, Va. : National Technical Information Service, distributor, 1992]

Series

NASA technical memorandum ; 105713

Reproduction

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

Added Author

Lambert, Heather H.

Mizukami, Masashi.

United States. National Aeronautics and Space Administration.

Gpo Item No.

0830-D (MF)

Sudoc No.

NAS 1.15:105713

Research Call Number

READEX Microfiche NAS 1.15:105713