Helicopterfixerman
24th Apr 2007, 16:37
Can someone please clarify something for me.?
I am of the mind that the "typical" open cockpit, flexiwing microlight aircraft is incapable of performing a loop in normal circumstances. My rational comes from teh combination of: Lack of turning moment since there is no elevator placed "x" distance from the CofG, the aircraft itself is little more than a flying wing with a gondola "pod" suspended beneath it, any deflection of the wing, i.e. angle of attack, will merely alter the amount of lift the wing generates rather than alter the nose up or down attitude of the "pod" and so in effect the whole aircraft either rises or sinks, the thrust from the engine is insufficient to provide enough momentum to achieve the roll, and any dive manouevre perfromed to aid in the build up of speed and thus momentum would ask questions of the structural integrity.
I would also like clarification that it cannot climb vertically, mainly for lack of thrust.
Am I right?
If I'm in the wrong section of the forum I apologise.
Many thanks in advance
HFM
I am of the mind that the "typical" open cockpit, flexiwing microlight aircraft is incapable of performing a loop in normal circumstances. My rational comes from teh combination of: Lack of turning moment since there is no elevator placed "x" distance from the CofG, the aircraft itself is little more than a flying wing with a gondola "pod" suspended beneath it, any deflection of the wing, i.e. angle of attack, will merely alter the amount of lift the wing generates rather than alter the nose up or down attitude of the "pod" and so in effect the whole aircraft either rises or sinks, the thrust from the engine is insufficient to provide enough momentum to achieve the roll, and any dive manouevre perfromed to aid in the build up of speed and thus momentum would ask questions of the structural integrity.
I would also like clarification that it cannot climb vertically, mainly for lack of thrust.
Am I right?
If I'm in the wrong section of the forum I apologise.
Many thanks in advance
HFM