Flight Investigation of Wing-Gun Fairings on a Fighter Type Airplane
Abstract
Description is given of flight tests conducted on gun fairings, designed to correct the detrimental effects of the projecting and submerged wing guns on an F4F-3 fighter. It was found that the installation of unfaired guns on a clean wing resulted in a premature stall that increased the stalling speed in the carrier-approach and landing conditions of flight by suitably fairing the guns, it was possible to reduce the stalling speeds to values approaching very nearly the clean-wing values.
Document Details
- Document Type
- Technical Report
- Publication Date
- Oct 01, 1941
- Accession Number
- ADA800761
Entities
People
- J. M. Nissen
- M. D. White
Organizations
- Langley Research Center