Balance Type Angle of Attack Indicator.
Abstract
The invention relates to an angle of attack indicator for use as a cock pit instrument including movable elements which respond to the differences in pressure at selected points on the aircraft. The pressure points include total pressure sensed by the aircraft pitot tube, atmospheric pressure sensed at aircraft static pressure port, and pressure sensed from at least one port on wing surface.
Document Details
- Document Type
- Technical Report
- Publication Date
- Aug 28, 1973
- Accession Number
- AD0164490
Entities
People
- R. W. Gallighton
Organizations
- United States Department of the Air Force