Wing-Body Combinations With Wings of Very Low Aspect Ratio at Supersonic Speeds Metadata
Metadata describes a digital item, providing (if known) such information as creator, publisher, contents, size, relationship to other resources, and more. Metadata may also contain "preservation" components that help us to maintain the integrity of digital files over time.
- Main Title Wing-Body Combinations With Wings of Very Low Aspect Ratio at Supersonic Speeds
- Series Title NACA Research Memorandums
Author: Jorgensen, Leland H.Creator Type: Personal
Author: Katzen, Elliott D.Creator Type: Personal
Originator: Ames Aeronautical Laboratory (U.S.)Contributor Type: OrganizationContributor Info: National Advisory Committee for Aeronautics. Ames Aeronautical Lab
- Creation: 1956-10-26
- Content Description: Memorandum presenting force and moment characteristics of configurations employing wings of very low aspect ratio have been determined for Mach numbers of 1.97 and 3.33. The angle-of-attack range was from 0 to 17 degrees for Mach number 1.97 and from 0 to 30 degrees for Mach number 3.33. The results of the investigation indicate that there are distinct aerodynamic advantages to the use of highly swept wings of very low aspect ratio.
- Physical Description: 62 p. : ill.
- Keyword: wing-body combinations
- Keyword: aircraft wings
Name: National Advisory Committee for Aeronautics CollectionCode: NACA
Name: Technical Report Archive and Image LibraryCode: TRAIL
Name: UNT Libraries Government Documents DepartmentCode: UNTGD
- Rights Access: public
- Rights License: pd
- Rights Statement: No Copyright, Unclassified, Unlimited, Publicly available
- Accession or Local Control No: 93R18725
- URL: http://hdl.handle.net/2060/19930089435
- Report No.: NACA-RM-A56G16
- Center for AeroSpace Information Number: 19930089435
- Archival Resource Key: ark:/67531/metadc62824