Robert Loewy
American scientist
Robert Loewy's AcademicInfluence.com Rankings
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Engineering Mathematics
Robert Loewy's Degrees
- PhD Physics Stanford University
Why Is Robert Loewy Influential?
(Suggest an Edit or Addition)According to Wikipedia, Robert Gustav Loewy is an aerospace engineer who has been influential in the development of rotary-wing vertical take-off and landing aircraft. He was born in Philadelphia, Pennsylvania. He graduated from Rensselaer Polytechnic Institute in the class of 1947 with a Bachelor of Aeronautical Engineering degree. He earned an M.S. from the Massachusetts Institute of Technology and a Ph.D. from the University of Pennsylvania. From 1948 to 1962, Dr. Loewy worked in industry for the Glenn L. Martin Company; Piasecki Helicopter Corporation; Cornell Aeronautical Laboratory; and Vertol Aircraft, which later became a division of the Boeing Company. Between September 1965 and 1966, he was chief scientist for the United States Air Force.
Robert Loewy's Published Works
Published Works
- REVIEW ARTICLE: Recent developments in smart structures with aeronautical applications (1997) (186)
- A Two-Dimensional Approximation to the Unsteady Aerodynamics of Rotary Wings (1957) (165)
- Helicopter Vibrations: A Technological Perspective (1984) (108)
- Theoretical Analysis of the Aerodynamic Stability of Multiple, Interdigitated Helical Vortices (1974) (99)
- Review of rotary-wing V/STOL dynamic and aeroelastic problems (1969) (38)
- Nonlinear analysis of pretwisted rods using 'principal curvature transformation'. I - Theoretical derivation (1987) (29)
- Dynamics of rotating shafts (1969) (27)
- Nonlinear Dynamics of Slender Rods (1987) (25)
- Uniaxial and Biaxial Fatigue Properties of Thin-Walled Composite Tubes (1988) (22)
- Structural dynamics of rotating bladed-disk assemblies coupled with flexible shaft motions (1984) (21)
- An Actuator-Disc Analysis of Helicopter Wake Geometry and the Corresponding Blade Response (1970) (21)
- Nonlinear analysis of pretwisted rods using 'principal curvature transformation'. II - Numerical results (1987) (19)
- Shaft flexibility effects on the forced response of a bladed-disk assembly (1990) (17)
- Modeling of Microcrack Damaged Composite Plates Undergoing Nonlinear Bimodular Flutter Oscillations (1998) (10)
- A THEORY FOR PREDICTING THE ROTATIONAL NOISE OF LIFTING ROTORS IN FORWARD FLIGHT, INCLUDING A COMPARISON WITH EXPERIMENT (1966) (10)
- Nonlinear aeroelastic effects in damaged composite aerospace structures (1997) (9)
- Structural dynamics studies of rotating bladed-disk assemblies coupled with flexible shaft motions (1983) (8)
- Aural Detection of Helicopters in Tactical Situations (1963) (8)
- Technical Notes: Influence of Pitch-Lag Coupling on Damping Requirements to Stabilize “Ground/Air Resonance” (1992) (6)
- Application of the principal curvature transformation to nonlinear rotor blade analysis (1986) (6)
- Unified treatment for dealing with auxiliary conditions in blade dynamics (1991) (5)
- Specialists Meeting on Helicopter Rotor Loads Prediction Methods (1973) (4)
- Helicopter Ground/Air Resonance Including Rotor Shaft Flexibility and Control Coupling (1989) (4)
- A matrix-Holzer analysis for bending vibrations of clustered launch vehicles. (1966) (4)
- SMART STRUCTURES STABILIZED UNSTABLE CONTROL SURFACES (1993) (4)
- Blade Mistuning Coupled With Shaft Flexibility Effects in Rotor Aeroelasticity (1989) (4)
- Matrix Holzer analyses for fully-coupled vibrations of clustered launch-vehicle configurations including applications to the Titan IIIC and uncoupled Saturn I cases (1966) (3)
- Shaft flexibility effects on aeroelastic stability of a rotating bladed disk (1989) (3)
- Transfer matrix analysis of cable-stiffened hoop platforms (1988) (2)
- Recent Studies of the Pitch-Lag Instabilities of Articulated Rotors (1961) (2)
- Natural frequency of rotating beams using non-rotating modes (1982) (2)
- Analytical Investigation of the Aerodynamic Stability of Helical Vortices Shed from a Hovering Rotor (1973) (2)
- Recent Studies on the Elastic Stability of Pretwisted Rods (1988) (2)
- Some Aeroelastic Problems of Tilt‐Wing; VTOL Aircraft (1958) (2)
- The importance of vortex shedding effects on helicopter rotor noise with and without blade slap. (1969) (2)
- Nonlinear analysis of anisotropic rods using curvature transformation and including warping (1991) (1)
- Composite structural materials. [aircraft structures] (1980) (1)
- Composite structural materials (2013) (1)
- Avionics - A 'new' senior partner in aeronautics (1999) (1)
- Transfer Matrix Vibration Analysis of Cable-Supported Hoop Platforms: Additional Results (1993) (1)
- A study of the influence of predeformations on the vibrations of blades (1990) (1)
- Avionics: A "New" Senior Partner in Aeronautics (1999) (1)
- Dynamic analysis of rotor blades with rotor retention design variations (1990) (0)
- Composite structural materials. [fiber reinforced composites for aircraft structures] (1981) (0)
- A FLIGHT INVESTIGATION OF THE EFFECTS OF BLADE ROOT MASS ON BLA45 2ENDING AND HELICOPTER VIBRATION LEVEL (1958) (0)
- THE 1999 AMA DRYDEN LECTURE AVIONICS: A "NEW' SENIOR PARTNER IN AERONAUTICS (1999) (0)
- 85 Years of Aeronautical/Aerospace Engineering at Georgia Tech: 1917-2002 (2003) (0)
- A MATRIX-HOLZER ANALYSIS FOR BENDING VIBRATIONS OF CLUSTERED LAUNCH VEHICLES (1965) (0)
- Structural dynamics and aeroelasticity of rotary wing aircraft (2000) (0)
- Formulation of a dynamic analysis method for a generic family of hoop-mast antenna systems (1981) (0)
- Biaxial fatigue properties of thin-walled composite tubes (1984) (0)
- Development of Unsteady Aerodynamic Prediction Techniques for High-Solidity Fans (2001) (0)
- "Smart structure" controlled aeroelastically unstable rotor (1995) (0)
- E-; c ,-x a 1 il = t Tests of an Unstable Lifting Surface Stabilized by a Simulated Smart Structure Introduction (2014) (0)
- Dynamic Analysis of Rotor Blades with Root Retention Design Variations (1992) (0)
- Composite structural materials. Annual progress report, 1 May 1985-30 April 1986 (1986) (0)
- Design analyses of 'hoop-maypole' satellite antennas using a mixed formulation (1992) (0)
- Guest Editorial: Helicopters, VTOL and Fuel Consumption (1981) (0)
- Composite structural materials. [aircraft applications (1981) (0)
- Studies of the Structural Dynamic Behavior of Satellite Antenna System. (1987) (0)
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