A Comparison of Wind Tunnel Data and Theoretical Predictions at M = 2.30, 2.60, and 2.96 for a Fighter with a Wing Having 74 Degrees of Sweep,
Document Details
- Document Type
- Technical Report
- Publication Date
- Oct 01, 1976
- Accession Number
- ADA955903
Entities
People
- Thomas M. Weeks
- William A. Sotomayer
Organizations
- Flight Dynamics Laboratory