EXPERIMENTAL RESEARCH OF NATURAL OSCILLATIONS OF A SQUARE PLATE IN A SUPERSONIC FLOW,
Abstract
Investigation is made of the natural oscillations (flutter) of a flat square plate in a supersonic flow at Mach 1.7, 2.3, and 3 for the case where two edges of the plate are perpendicular to the flow and fastened and two edges parallel to the flow are open. The results of the experiment are compared with a theoretical solution. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Mar 09, 1965
- Accession Number
- AD0612415
Entities
People
- G. N. Mikishev
Organizations
- National Air and Space Intelligence Center