Users Manual for Tilt-Wing and Deflected Slipstream Aerodynamics Program,
Abstract
A digital computer program was developed for the purpose of estimating the aerodynamic lift, longitudinal forces and pitching moment characteristics of a tilt-wing or deflected slip-stream V/STOL configuration. Punched card output from this program provides the aerodynamic input data to the performance program for calculating takeoffs, landings and transitions of V/STOL aircraft. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- May 28, 1970
- Accession Number
- AD0745366
Entities
People
- S. K. Pederson
Organizations
- General Dynamics