Flight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds
We couldn't estimate the reading time for this book.
Author
Contributions
- Lamar, John E. - Contributor
- Langley Research Center. - Contributor
Publication
2001 - National Aeronautics and Space Administration, Langley Research Center, Hampton, Va, Virginia
Language
English
Word Count
0 words, Guess
Page Count
0 pages
Identifiers
- Open LibraryOL17610253M
- OCLC Control Number51617379
Alternate Titles
- Flight, wind tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds.
Subjects
Series Statement
- NASA/TP -- 2001-210629.
Reader Reviews
No reviews yet for this book.
Be the first to share your thoughts!