Tests of Republic 320-Gal Tip Tanks on an F-84G
Abstract
Flight tests were conducted on an F-84G to evaluate the drag and the maneuvering flight characteristics of the aircraft with modified Republic 320- gal experimental tip tanks installed. Vibratory accelerations experienced by the 320-gal tanks and the tank center-of-gravity shift with attitude change and time were also measured. Compared with Republic standard 230-gal tip tanks, the modified 320-gal tanks were found to indicate (1) an additional loss at 10,000 ft of some 3 to 7 knots calibrated air speed in the rpm range max continuous to 84% (2) the same or slightly higher stick forces in maneuvering flight.
Document Details
- Document Type
- Technical Report
- Publication Date
- Oct 07, 1954
- Accession Number
- AD0858286
Entities
People
- H. R. Miller