Rotary Derivatives of a Delta Wing at Supersonic Speeds
- 1 February 1948
- journal article
- research article
- Published by Cambridge University Press (CUP) in Journal of the Royal Aeronautical Society
- Vol. 52 (455) , 735-752
- https://doi.org/10.1017/s0368393100101981
Abstract
Summary The rotary derivatives of a Delta wing pitching or rolling at supersonic speed are obtained in addition to the lift curve slope first given in an earlier investigation.Keywords
This publication has 1 reference indexed in Scilit:
- The lift of a delta wing at supersonic speedsQuarterly of Applied Mathematics, 1946