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Canards
Close coupled or long arm?
What is canard
French for “duck”
Ducks have a layer of feathers around the
neck which improves aerodynamics
Canard is a control surface in front of the
wing
Lifting canard
Control canard
General effects
Loaded canard decreased drag at
supersonic speeds
Provides upload vs traditional tail download
Reduced need for elevon trim
Less drag in level flight
Unloaded canard only adds minor drag,
but improves lift and reduces drag in turn
Improved STOL performance
Close coupled canard
Increases instability level
Low pressure area at forward part of the wing
> dynamic instability
Does not shift to stability during supersonic flight
Improved pitch rate through angle of attack
range
Improved pitch onset and turn onset rate
Close coupled canard
Improved lift at high angles of attack
Improved instantaneous turn rate
Little effect at speeds above Mach 0,9
Reduced necessary wing twist
Reduced drag for a given angle of attack
Delayed stall; reduced trim drag
Significant improvement in L/D ratio
Close coupled canard
Vortexes improve wing response to control
surface inputs and improve control surface
effectiveness
Improved transient performance
Roll onset rate in particular
Improved control effectiveness at high angles
of attack
Close coupled canard
Reduced drag during supersonic cruise
Reduced centre of lift shift
Less trim drag
No effect on lift or drag during supersonic
maneuvers
Stall and spin recovery
Long arm canard
Canard vortex bursts early due to lack of
influence from the parent wing
No drag improvement at high AoA
No improvement in roll onset rate
Lift improvement limited to increase in
reference area caused by addition of canard;
no effect on the parent wing
Requires greater static instability margin to
achieve same overall amount of instability >
no dynamic instability
Conclusions
Close coupled canard is a better choice for
applications where maneuverability is
required
Long arm canard may be better for cruise
performance
Both canard configurations are superior to
a traditional wing-tail configuration
Presentation by Picard578
http://defenseissues.wordpress.com/
http://defenseissues.wordpress.com/2014/08/23/close-coupled-vs-long-arm-canard/

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Canards

  • 2. What is canard French for “duck” Ducks have a layer of feathers around the neck which improves aerodynamics Canard is a control surface in front of the wing Lifting canard Control canard
  • 3. General effects Loaded canard decreased drag at supersonic speeds Provides upload vs traditional tail download Reduced need for elevon trim Less drag in level flight Unloaded canard only adds minor drag, but improves lift and reduces drag in turn Improved STOL performance
  • 4.
  • 5. Close coupled canard Increases instability level Low pressure area at forward part of the wing > dynamic instability Does not shift to stability during supersonic flight Improved pitch rate through angle of attack range Improved pitch onset and turn onset rate
  • 6. Close coupled canard Improved lift at high angles of attack Improved instantaneous turn rate Little effect at speeds above Mach 0,9 Reduced necessary wing twist Reduced drag for a given angle of attack Delayed stall; reduced trim drag Significant improvement in L/D ratio
  • 7. Close coupled canard Vortexes improve wing response to control surface inputs and improve control surface effectiveness Improved transient performance Roll onset rate in particular Improved control effectiveness at high angles of attack
  • 8. Close coupled canard Reduced drag during supersonic cruise Reduced centre of lift shift Less trim drag No effect on lift or drag during supersonic maneuvers Stall and spin recovery
  • 9. Long arm canard Canard vortex bursts early due to lack of influence from the parent wing No drag improvement at high AoA No improvement in roll onset rate Lift improvement limited to increase in reference area caused by addition of canard; no effect on the parent wing Requires greater static instability margin to achieve same overall amount of instability > no dynamic instability
  • 10. Conclusions Close coupled canard is a better choice for applications where maneuverability is required Long arm canard may be better for cruise performance Both canard configurations are superior to a traditional wing-tail configuration