UNIFIED ANALYSIS OF AERODYNAMIC LOADS AT SUPERSONIC SPEEDS ON TRIANGULAR WINGS HAVING ARBITRARY CAMBER AND TWIST. VOLUME II,
Abstract
The report consists primarily of data in graphical form. In addition, general delta wing characteristics and tabulated parameters are given.
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 20, 1956
- Accession Number
- AD0697866
Entities
People
- Helen M. Grijalva
- Julian H. Kainer
Organizations
- General Dynamics