Performance of twin-dimensional wedge nozzles including thrust vectoring and reversing effects at speeds up to Mach 2.20
(Book)

Book Cover
Average Rating
Author
Capone, Francis J.
Contributors
Maiden, Donald L., author.
Langley Research Center.
United States. National Aeronautics and Space Administration
Published
Washington : National Aeronautics and Space Administration ;, 1977.
Physical Desc
1 unnumbered page, 188 pages : illustrations ; 27 cm.
Status
Available from another library
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Description

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Copies

LocationCall NumberStatus
Indiana State Library - Indianapolis - General Federal documentsNAS 1.14:D-8449On Shelf

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Subjects

LC Subjects
Jet nozzles.
Jet planes -- Thrust reversers.

More Details

Published
Washington : National Aeronautics and Space Administration ;, 1977.
Format
Book
Language
English

Notes

General Note
Prepared at Langley Research Center, Hampton, Va.
General Note
Sponsored by the National Aeronautics and Space Administration, Washington, D.C.
General Note
Report date: July 1977.
Bibliography
Includes bibliographical references.

Citations

APA Citation, 7th Edition (style guide)

Capone, F. J., & Maiden, D. L. (1977). Performance of twin-dimensional wedge nozzles including thrust vectoring and reversing effects at speeds up to Mach 2.20 . National Aeronautics and Space Administration ;.

Chicago / Turabian - Author Date Citation, 17th Edition (style guide)

Capone, Francis J and Donald L., Maiden. 1977. Performance of Twin-dimensional Wedge Nozzles Including Thrust Vectoring and Reversing Effects At Speeds Up to Mach 2.20. National Aeronautics and Space Administration.

Chicago / Turabian - Humanities (Notes and Bibliography) Citation, 17th Edition (style guide)

Capone, Francis J and Donald L., Maiden. Performance of Twin-dimensional Wedge Nozzles Including Thrust Vectoring and Reversing Effects At Speeds Up to Mach 2.20 National Aeronautics and Space Administration, 1977.

MLA Citation, 9th Edition (style guide)

Capone, Francis J., and Donald L. Maiden. Performance of Twin-dimensional Wedge Nozzles Including Thrust Vectoring and Reversing Effects At Speeds Up to Mach 2.20 National Aeronautics and Space Administration ;, 1977.

Note! Citations contain only title, author, edition, publisher, and year published. Citations should be used as a guideline and should be double checked for accuracy. Citation formats are based on standards as of August 2021.

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