Publication Date:
2019-07-13
Description:
High-angle-of-attack flight dynamics of the X-29 configuration were studied using dynamic model test techniques. These tests identified phenomena including wing rock, spins, and tumbling which dominate the high-alpha behavior of the configuration and define its usable flight envelope. Results of these tests have been used to design flight control concepts to minimize adverse behavior. Planned high-angle-of-attack flight tests of the X-29 airplane will provide an opportunity to validate the model predictions.
Keywords:
AIRCRAFT STABILITY AND CONTROL
Type:
SAE PAPER 881420
,
Aerospace Technology Conference and Exposition; Oct 03, 1988 - Oct 06, 1988; Anaheim, CA; United States
Format:
text
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