Research Catalog

Details

Additional authors

1. Lewis Research Center, issuing body.
2. United States. National Aeronautics and Space Administration, sponsoring body.

Description

1. 1 online resource (13 pages) : illustrations.

Series statement

1. NASA technical memorandum ; 107288

Uniform title

1. NASA technical memorandum ; 107288.

Subject

1. Engine design
2. Structural weight
3. Structural design
4. Supersonic inlets
5. Finite element method
6. Air intakes
7. Symmetry

Call number

1. GPO Internet NAS 1.15:107288

Note

1. Title from title screen (viewed April 20, 2016).
2. "Prepared for the 32nd Joint Propulsion Conference cosponsored by AIAA, ASME, SAE, and ASEE, Lake Buena Vista, Florida, July 1-3, 1996."
3. "Performing organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page.

Bibliography (note)

1. Includes bibliographical references (page 9).

Funding (note)

1. Sponsored by the National Aeronautics and Space Administration

Author

1. Nadell, Shari-Beth, author.

Title

1. Minimum weight design of a generic axisymmetric inlet / Shari-Beth Nadell.

Publisher

1. Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, August 1996.

Type of content

1. text

Type of medium

1. computer

Type of carrier

1. online resource

Series

1. NASA technical memorandum ; 107288
2. NASA technical memorandum ; 107288.

Bibliography

1. Includes bibliographical references (page 9).

Funding

1. Sponsored by the National Aeronautics and Space Administration WU-505--69-50 E-10363 AIAA-96-2550

Connect to:

1. https://purl.fdlp.gov/GPO/gpo67123

Added author

1. Lewis Research Center, issuing body.
2. United States. National Aeronautics and Space Administration, sponsoring body.

Other form:

1. Microfiche version: Nadell, Shari-Beth. Minimum weight design of a generic axisymmetric inlet (OCoLC)39668406

Gpo item no.

1. 0830-D (online)

Sudoc no.

1. NAS 1.15:107288