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F-14A High-Angle-of-Attack Characteristics

Authors: William Bihrle; Rudolph C. Meyer;

F-14A High-Angle-of-Attack Characteristics

Abstract

The F-14 has demonstrated that fighter aircraft can be designed to have no lift curve break or angle-of-attack limitation. The maneuver flight envelope, therefore, has been expanded beyond what had traditionally been considered possible. The value of this high alpha capability in the dogfight arena has been convincingly demonstrated in flight. The importance of slats and an ARI system for enhancing this capability has also been demonstrated. The development from concept through flight test of this high alpha capability is presented by candidly reviewing the design philosophy, the background that dictated it, and the results of experimental and analytical studies.

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Powered by OpenAIRE graph
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selected citations
These citations are derived from selected sources.
This is an alternative to the "Influence" indicator, which also reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).
BIP!Citations provided by BIP!
popularity
This indicator reflects the "current" impact/attention (the "hype") of an article in the research community at large, based on the underlying citation network.
BIP!Popularity provided by BIP!
influence
This indicator reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).
BIP!Influence provided by BIP!
impulse
This indicator reflects the initial momentum of an article directly after its publication, based on the underlying citation network.
BIP!Impulse provided by BIP!
2
Average
Top 10%
Average
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