Aerodynamic loading of wings. File Ma 8/8/02. The Fairey Aviation Co. Ltd. Technical Office Report 206. The Sequence of Calculations required for the Richardson Theory of Lifting Forces on Wings. Appendix II. Technical Report No. 165, Method for calculation the lifting forces on wings by J.R. Richardson. Report: Aerodynamic loading on an oscillating wing at supersonic speeds, Hawker Aircraft T.N. 19. Bristol Aircraft Ltd. Technical Note No. M8, Notes on D.E.U.C.E. programmes for the computation of Flutter coefficients using the Multhopp-Garner Theory by K.G. Blackmore. Paper: Supersonic Lift Distribution on a 70� Delta Wing by J.R. Richardson. MD/TDO/JRR/IJM. Paper: On the programming of Falkner-Jones calculations for a digital machine by P.M. Stocker. Ae/A/200. Various papers and calculations on aerodynamics in supersonic potential flow in wing design.

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