The work presented in this report is a continuation of work started under NASC Contract No. 00019-68-C-0274, Collocation Flutter Analysis Study. This work, which is presented in three volumes, is to update and document computer automated flutter analysis techniques. This volume contains subsonic strip theory unsteady aerodynamics program (Strip), and supersonic piston theory unsteady aerodynamics program (Piston). (Author)
Collocation Flutter Analysis Study II (COFA II). Volume I. Subsonic Strip Theory Unsteady Aerodynamics Program. Supersonic Piston Theory Unsteady Aerodynamics Program
1970
79 pages
Report
No indication
English
Manned Spacecraft , Fluid Mechanics , Aerospace planes , Aerodynamic control surfaces , Flutter , Aerodynamic characteristics , Mathematical models , Vibration , Sweptback wings , Variable sweep wings , Subsonic characteristics , Supersonic characteristics , Aerodynamic loading , Angle of attack , Computer programming , Computer programs , Theory , Collocation flutter , Piston theory , Strip theory
New Look at Unsteady Supersonic Potential Flow Aerodynamics and Piston Theory
Online Contents | 2015
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