Aerodynamic forces on a cylindrical shell in panel flutter,
Saved in:
Corporate author / creator: | Brown University. Division of Applied Mathematics |
---|---|
Imprint: | Providence, 1958. |
Description: | 12 p. illus. |
Language: | English |
Subject: | |
Format: | Print Book |
URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/4171522 |
Other authors / contributors: | Holt, Maurice United States. Air Force. Office of Scientific Research. |
---|---|
Notes: | Paper read at the Mechanics Division AFOSR Contractors Meeting, Kansas City Mo., Oct. 23-24, 1958. Sponsored by the Air Force Office of Scientific Research under Contract AF 49(638)-232. AFOSR TN-58-974; AD 205 598. |
Similar Items
-
Elastic stability of circular cylindrical shells /
by: Yamaki, N. (Noboru), 1920-
Published: (1984) -
Flutter of thin panels at subsonic and supersonic speeds (U) /
by: Greenspon, Joshua E.
Published: (1957) -
Bending of cylindrical shells solution using cylindrical strip elements [and] Finite element analysis of cylindrical shells solution using rectangular circular cylindrical elements.
by: Jiroušek, Jaroslav
Published: (1970) -
Note on the resistance of polished cylinders (and cylindrical wires) with generatrices perpendicular to the airstream /
by: Toussaint, A.
Published: (1921) -
Method for experimental determination of flutter speed by parameter identification /
by: Nissim, E.
Published: (1989)