A Study of the Damping Characteristics on Models of Supersonic Airlines at Supersonic Speeds,
Abstract
The article presents the results of an experimental study of the damping moment coefficients of the configuration of supersonic airliner models with small wing aspect ratios in a supersonic wind tunnel. A comparison of experimental and calculated data is presented.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jul 24, 1974
- Accession Number
- AD0784259
Entities
People
- M. V. Ushakov
- N. N. Tyunin
Organizations
- National Air and Space Intelligence Center