Wind-Tunnel Investigation of a Plain Aileron with Various Trailing Edge Modifications on a Tapered Wing. 3 - Ailerons with Simple and Spring-Linked Balancing Tabs
Abstract
Aerodynamics data are obtained for the design of linked balancing tabs and effect of varied tab span and location to produce suitable lateral control characteristics with reasonable stick pressures for high-speed aircraft. Simple and spring-linked balancing tabs may considerably reduce control pressures if aileron system is designed for low maximum aileron deflection. Spring-linked tabs also decrease variation of stick pressure with speed and impart better controlllability at low speeds.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 01, 1943
- Accession Number
- ADA800589
Entities
People
- F. M. Rogallo
- Paul E. Purser
Organizations
- Langley Research Center