<BLOCKQUOTE id=quote><font size=1 face="Verdana, Arial, Helvetica" id=quote>quote:<hr height=1 noshade id=quote>incidence, <hr height=1 noshade id=quote></BLOCKQUOTE id=quote></font id=quote><font face="Verdana, Arial, Helvetica" size=2 id=quote>
incedence is the relationship of the Main wing to the rear horizontal stabiliser (parallel)
When talking airfoild, the ailerons dependent on the design may creat more Lift pressure, but they also induce drag.
once you input deflection down on the right side it inputs and opposite direction topside of the left wing. This creates "Roll" axis.
By adjusting your Horizontal stabiliser and maintaining a specified amount of "AOA" and thrust you can maintain a level inverted flight. Although it is dependent to the induced drag, excessive AOA and minute thrust will not over come the drag.
Everybody has done this from time to time, Sticking your hand outside the window of a moveing car and flying it as an airfoil in the airflow. Causeing your hand to rise or decend. But if you require a specified ammount of "AOA" at slower speeds to do this, it requires more aoa and has a higher drag index.
This is a good discription of a Flatbottom airfoil.
A fully semetrical airfoil which has an equildistant radius at top mean chord and bottom tapering to the trailing edge, would require signifigant AOA on slower speeds to maintain lift until sufficent speed creates the dynamic pressure to level the flight.
It is the same principle for an arrow, if it doesnt provide sufficient positive AOA in flight then your arrow fals short becasue it fails to maintain thrust and lift, although the dynamic pressure allows it to escape gravity for a short period of time.
The same goes for a rocket.
The a10 has a "Semi Semetrical under camber wing" this design provides great ammount of lift with minimal amount of drag, becasue of the semisemetrical leading edge (reduces Drag) and the rear undercamber Generates lift. Incorporated with the flaps It creats a high amount of lift vaccuum and the tradeoff is a great deal of lag.
here are some sites of intrest
Free airfoil program
http://www.ctaz.com/~kelcomp/airfoils5.htm
Other Free ware NACA airfoil formulas and ratios, programs.
http://www.pdas.com/naca456.htm
"The power to Destroy the planet, is insignifigant to the power of the Air Force----Mudd Vader