Pressure distributions from subsonic tests of an advanced laminar-flow-control wing with leading- and trailing-edge flaps
We couldn't estimate the reading time for this book.
Author
Contributions
- Gentry, Garl L. - Contributor
- United States. National Aeronautics and Space Administration. Scientific and Technical Information Division. - Contributor
Publication
1988 - For sale by the National Technical Information Service], Washington, D.C., District of Columbia
Language
English
Word Count
0 words, Guess
Page Count
0 pages
Physical Format
Microform
Identifiers
- Open LibraryOL17660077M
Subjects
Topics
Series Statement
- NASA technical memorandum -- 4040.
Other Editions
- Pressure distributions from subsonic tests of an advanced laminar-flow-control wing with leading- and trailing-edge flaps
Reader Reviews
No reviews yet for this book.
Be the first to share your thoughts!