- Restrictions on Access:
- Unclassified, Unlimited, Publicly available.
- 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.
- NASA Technical Reports Server (NTRS) Collection.
- Document ID: 19760022068.
Accession ID: 76N29156.
- No Copyright.
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