ICAS-92-6.6.2 Aeroelastic Stability Characteristics of Composite Cylindrical Shells by the Finite Element Method
18th Congress ; 1992 ; Beijing
01.01.1992
9 pages
In 2 vols
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Aeroelastic Stability Characteristics of Composite Cylindrical Shells by the Finite Element Method
British Library Online Contents | 1992
|ICAS-92-5.9.4 Aeroelastic Analysis of Composite Wing with Control Surface
British Library Conference Proceedings | 1992
|