Propulsion Study for STOL Air-Sea Craft.
Abstract
The purpose of the study was to investigate aerodynamic-propulsion concepts applicable to the canard configuration STOL air-sea craft, and in particular to develop and use a methodology for optimizing combinations of direct lift and augmented wing lift. A computer program was developed that optimized the propulsion system by maximizing the airplane radius for a given mission and a fixed initial airplane weight. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 15, 1969
- Accession Number
- AD0862843
Entities
People
- Alan C. Brown
- Arthur B. Anderson
- Edward H. Hohman
Organizations
- Lockheed Martin