Explore: Sweptback Wings
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Books Results
Source: The Open Library
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1Two experimental supercritical laminar-flow-control swept-wing airfoils
By Dennis O. Allison
“Two experimental supercritical laminar-flow-control swept-wing airfoils” Metadata:
- Title: ➤ Two experimental supercritical laminar-flow-control swept-wing airfoils
- Author: Dennis O. Allison
- Language: English
- Number of Pages: Median: 22
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1987
- Publish Location: [Springfield, Va - Hampton, Va
“Two experimental supercritical laminar-flow-control swept-wing airfoils” Subjects and Themes:
- Subjects: ➤ Transonic wind tunnels - Sweptback wings - Laminar flow airfoils - Supercritical airfoils - Wind tunnel tests - Aerofoils
Edition Identifiers:
- The Open Library ID: OL15407161M
Access and General Info:
- First Year Published: 1987
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
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2Experimental and theoretical study of the longitudinal aerodynamic characteristics of delta and double-delta wings at mach numbers of 1.60, 1.90, and 2.16
By Richard M. Wood
“Experimental and theoretical study of the longitudinal aerodynamic characteristics of delta and double-delta wings at mach numbers of 1.60, 1.90, and 2.16” Metadata:
- Title: ➤ Experimental and theoretical study of the longitudinal aerodynamic characteristics of delta and double-delta wings at mach numbers of 1.60, 1.90, and 2.16
- Author: Richard M. Wood
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service
- Publish Date: 1985
- Publish Location: ➤ Springfield, Va - [Washington, D.C.]
“Experimental and theoretical study of the longitudinal aerodynamic characteristics of delta and double-delta wings at mach numbers of 1.60, 1.90, and 2.16” Subjects and Themes:
- Subjects: Delta wings - Supersonic flow - Sweptback wings - Supersonic airfoils
Edition Identifiers:
- The Open Library ID: OL17724282M
Access and General Info:
- First Year Published: 1985
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Experimental and theoretical study of the longitudinal aerodynamic characteristics of delta and double-delta wings at mach numbers of 1.60, 1.90, and 2.16 at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.