2007 - Spirit of St. Louis Medal, The American Society of Mechanical Engineers
1993 - Fellow of the American Society of Mechanical Engineers
1993 - Member of the National Academy of Engineering For contributions to aeroelasticity and structural dynamics, which provide continuing insights into the behavior of complex structural systems.
Earl H. Dowell mainly focuses on Aeroelasticity, Flutter, Mechanics, Aerodynamics and Nonlinear system. His Aeroelasticity study also includes
As a part of the same scientific study, Earl H. Dowell usually deals with the Mechanics, concentrating on Classical mechanics and frequently concerns with Vibration, Harmonic balance and Föppl–von Kármán equations. His work deals with themes such as Computational fluid dynamics, Airfoil, Vortex, Helicopter rotor and Wind tunnel, which intersect with Aerodynamics. His Nonlinear system research includes elements of Bending of plates, Geometry, Chord and Boundary layer.
His primary areas of study are Aeroelasticity, Mechanics, Flutter, Nonlinear system and Aerodynamics. His study on Aeroelasticity also encompasses disciplines like
His Flutter study combines topics from a wide range of disciplines, such as Limit cycle, Structural engineering, Plate theory, Supersonic speed and Stall. His work in Nonlinear system tackles topics such as Mathematical analysis which are related to areas like Modal analysis. His studies in Aerodynamics integrate themes in fields like Potential flow and Computational fluid dynamics.
The scientist’s investigation covers issues in Mechanics, Nonlinear system, Aeroelasticity, Flutter and Mathematical analysis. His Mechanics course of study focuses on Cantilever and Boundary value problem and Beam. His research in Nonlinear system intersects with topics in Algorithm, Aerodynamics and Equations of motion.
His research on Aeroelasticity also deals with topics like
Mechanics, Nonlinear system, Aeroelasticity, Equations of motion and Flutter are his primary areas of study. Earl H. Dowell has included themes like Vibration and Thrust-to-weight ratio in his Mechanics study. The concepts of his Nonlinear system study are interwoven with issues in Partial differential equation, Mathematical analysis, Buckling, Normal mode and Transient response.
His study in Aeroelasticity is interdisciplinary in nature, drawing from both Acoustics, Piezoelectricity, Control theory, Harmonic balance and Wind tunnel. His work investigates the relationship between Flutter and topics such as Structural engineering that intersect with problems in Flow velocity. His Aerodynamics study integrates concerns from other disciplines, such as Airfoil, Restoring force and Reduced frequency.
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A Modern Course in Aeroelasticity
E. H. Dowell;R. M. Bennett;H. C. Curtiss;R. H. Scanlan.
(1989)
Aeroelasticity of Plates and Shells
E. H. Dowell;Holt Ashley.
(1974)
Nonlinear equations of motion for the elastic bending and torsion of twisted nonuniform rotor blades
D. H. Hodges;E. H. Dowell.
(1974)
Modeling of Fluid-Structure Interaction
Earl H Dowell;Kenneth C Hall.
Annual Review of Fluid Mechanics (2001)
Nonlinear oscillations of a fluttering plate. II.
Earl H. Dowell.
AIAA Journal (1966)
Acoustoelasticity - General theory, acoustic natural modes and forced response to sinusoidal excitation, including comparisons with experiment
E.H. Dowell;G.F. Gorman;D.A. Smith.
Journal of Sound and Vibration (1977)
Parametric Random Vibration
R. A. Ibrahim;T. Fang;E. H. Dowell.
(1985)
Panel flutter - A review of the aeroelastic stability of plates and shells
E. H. Dowell.
AIAA Journal (1970)
Localization of vibrations by structural irregularity
C. Pierre;E.H. Dowell.
Journal of Sound and Vibration (1987)
Nonlinear Inviscid Aerodynamic Effects on Transonic Divergence, Flutter, and Limit-Cycle Oscillations
Jeffrey P. Thomas;Earl H. Dowell;Kenneth C. Hall.
AIAA Journal (2002)
Journal of Fluids and Structures
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