cranfield0060

estim forc moment due roll sever slender tail configur superson speed veloc potenti span load correspond forc moment deriv theoret evalu number slender tail arrang perform steadi roll motion superson speed method analysi base upon applic conformaltransform techniqu util techniqu allow simpl determin complex potenti variou type two dimension boundari valu problem addit two simpl often use approxim roll deriv compar correspond exact valu determin method present report order show import wing tail interfer effect flow field behind roll wing tail characterist illustr simpl wing tail arrang