The Effect of Span and Deflection of Split Flaps and Leading-edge Roughness on the Longitudinal Stability and Gliding Characteristics of a 42 Degree Sweptback Wing Equipped with Leading-edge Flaps
1949-06-21
Miscellaneous
No indication
English
Analysis of a delta wing with leading-edge flaps
AIAA | 1987
|ACTUATOR ASSEMBLIES TO DEPLOY AIRCRAFT LEADING EDGE FLAPS AND SEALS FOR AIRCRAFT LEADING EDGE FLAPS
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|Actuator assemblies to deploy aircraft leading edge flaps and seals for aircraft leading edge flaps
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