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Angle of Attack as an Aid to Flying

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Tuomela, Commander C. H., author.
Conference Name:
National Aeronautic Meeting and Production Forum (1965-04-12 : Washington, District of Columbia, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1965
Summary:
Application of the early ideas of Wilbur and Orville Wright, in regards to angle of incidence, has provided the Navy with an effective method of controlling airplane approach and landing speeds. The current Navy angle-of-attack systems have commercial applications for use in landing, clear air turbulence, stall warning and other flight regimes. The most important application of the angle-of-attack, to date, has been its use with automatic throttle for control of speed in approaches and landings. The angle-of-attack system provides optimum reference for auto-throttle operation regardless of aircraft weight, bank angle, flap settings, "g" loading and engines in operation
Notes:
Vendor supplied data
Publisher Number:
650250
Access Restriction:
Restricted for use by site license

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