ANALYSIS OF TURBOJET AIRPLANE DRAG AND FUEL CONSUMPTION DATA.
Abstract
Level flight cruise performance of turbojet airplane is discussed in detail. The W/delta and RNI methods of data analysis are presented with a discussion of limitations and advantages. Typical drag, engine and specific range curves are presented. Non-standard temperature and wind corrections to specific range are also included. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Oct 16, 1961
- Accession Number
- AD0649580
Entities
People
- F. L. Goebel
Organizations
- Naval Air Station Patuxent River