Pressure Driven Angle of Attack Indicating System.
Abstract
Technically inclined flyers have long recognized the importance to the pilot of angle of attack information. Unfortunately, a reliable, accurate, and low cost angle of attack indicator has not been available. From the outset, the goal of this research has been to develop an angle of attack indicator as simple, accurate, reliable, and inexpensive as the common airspeed indicator so that it could be used as a primary landing approach aid and for the other flight control functions. This report describes the solution to that problem.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 01, 1976
- Accession Number
- ADA035321
Entities
People
- James W. Christian
- Roger W. Gallington
Organizations
- United States Air Force Academy