A strip method for prediction of damping in subsonic wind tunnel andflight flutter tests.
- 1 January 1969
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 6 (1) , 9-17
- https://doi.org/10.2514/3.43994
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- A method for deriving structural influence coefficients from ground vibration tests.AIAA Journal, 1967
- Modified-strip-analysis method for predicting wing flutter at subsonic to hypersonic speeds.Journal of Aircraft, 1966
- A MORE REALISTIC METHOD FOR ROUTINE FLUTTER CALCULATIONSPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1965
- QUASI-STATIC AERO-THERMO-ELASTIC ANALYSIS: ANALYTICAL DEVELOPMENT AND COMPUTATIONAL PROCEDUREPublished by Defense Technical Information Center (DTIC) ,1963
- Readers ForumJournal of the Aerospace Sciences, 1961
- Über die Entstehung des dynamischen Auftriebes von TragflügelnZAMM - Journal of Applied Mathematics and Mechanics / Zeitschrift für Angewandte Mathematik und Mechanik, 1925