ON WING-BODY INTERACTION AT SUPERSONIC SPEEDS II,
Abstract
The shape of the pressure curve on the root chord of a wing, extending symmetrically from a fuselage of circular cylindrical cross-section and near its leading edge was calculated. The wing is assumed to have non-zero thickness and can be at incidence. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 13, 1967
- Accession Number
- AD0663149
Entities
People
- K. Stewartson
Organizations
- University College London