Analysis of information sources in references of the Wikipedia article "Canard (aeronautics)" in English language version.
{{citation}}: CS1 maint: multiple names: authors list (link)....the Flyer was highly unstable... The lateral/directional stability and control of the Flyer were marginal.
Incorporating roll control on the canard is basically less efficient because of an adverse downwash influence on the main wing opposing the canard rolling-moment input.
...the Flyer was highly unstable... The lateral/directional stability and control of the Flyer were marginal.
Incorporating roll control on the canard is basically less efficient because of an adverse downwash influence on the main wing opposing the canard rolling-moment input.
...the Flyer was highly unstable... The lateral/directional stability and control of the Flyer were marginal.
Incorporating roll control on the canard is basically less efficient because of an adverse downwash influence on the main wing opposing the canard rolling-moment input.
Incorporating roll control on the canard is basically less efficient because of an adverse downwash influence on the main wing opposing the canard rolling-moment input.
On the Wright brother's first aircraft, the horizontal stabilizer was placed in front of the wings.
The X-29... while its canards—horizontal stabilizers to control pitch—were in front of the wings instead of on the tail.
...a front stabilizer, generally known as a canard stabilizer…
{{citation}}: CS1 maint: multiple names: authors list (link).{{cite web}}: |last= has generic name (help)On the Wright brother's first aircraft, the horizontal stabilizer was placed in front of the wings.