Theoretical and experimental panel flutter studies in the Mach number range 1.0 to 5.0.
- 1 December 1965
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 3 (12) , 2292-2304
- https://doi.org/10.2514/3.3359
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- FLUTTER ANALYSIS OF FLAT RECTANGULAR PANELS BASED ON THREE-DIMENSIONAL SUPERSONIC POTENTIAL FLOWAIAA Journal, 1963
- THE EFFECT OF A CAVITY ON PANEL VIBRATIONAIAA Journal, 1963
- Flutter of Rectangular Simply Supported Panels at High Supersonic SpeedsJournal of the Aeronautical Sciences, 1957
- THEORETICAL STUDIES ON THE PREDICTION OF UNSTEADY SUPERSONIC AIRLOADS ON ELASTIC WINGS. PART I. INVESTIGATIONS ON THE USE OF OSCILLATORY SUPERSONIC AERODYNAMIC INFLUENCE COEFFICIENTSPublished by Defense Technical Information Center (DTIC) ,1955
- The Vibration of Rectangular PlatesProceedings of the Institution of Mechanical Engineers, 1954