Effect of wing-tip dihedral on the longitudinal and lateral aerodynamic characteristics of a supersonic cruise configuration at subsonic speeds
- Author:
- Gloss, B. B.
- Published:
- Aug 1, 1976.
- Physical Description:
- 1 electronic document
- Additional Creators:
- Washburn, K. E.
- Access Online:
- hdl.handle.net
- Restrictions on Access:
- Unclassified, Unlimited, Publicly available.
- Summary:
- Force and moment data studies were conducted to determine the effect of wing-tip dihedral on the longitudinal and lateral aerodynamic characteristics of a supersonic cruise fighter configuration. Oil flow studies were also performed to investigate the model surface flow. Three models were tested: a flat (0 deg dihedral) wing tip, a dihedral, and an anhedral wing tip. The tests were conducted at the NASA Langley high-speed 7- by 10-foot wind tunnel.
- Collection:
- NASA Technical Reports Server (NTRS) Collection.
- Note:
- Document ID: 19760022068.
Accession ID: 76N29156.
NASA-TM-X-72693. - Terms of Use and Reproduction:
- No Copyright.
- Access Online:
- hdl.handle.net
View MARC record | catkey: 15734983