Supersonic Cruise/Transonic Maneuver Wing Section Development Study.
Abstract
Computational aerodynamic design of advanced fighter wings with well-controlled transonic maneuver flow and high supersonic cruise efficiency is described. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 01, 1980
- Accession Number
- ADA110686
Entities
People
- Ellwood Bonner
- Philip Gingrich