Author

R. L. Palko

Observed names: Palko, R. L., Palko, R. L., author., Palko, Richard L., author., R. PALKO

Observed institution: United States Air Force

OpenAlex ID: A5076381111

Documentation of ice shapes on the main rotor of a UH-1H helicopter in hover

1984 · J. D. Lee, Richard Harding, et al. · NASA STI Repository (National Aeronautics and Space Administration) · 14

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In-flight photogrammetric measurement of wing ice accretions

1986 · R. MCKNIGHT, R. PALKO, et al. · 24th Aerospace Sciences Meeting · 7

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Tests of an improved, computer-controlled, self-optimizing, variable-geometry wing

1982 · E. LEVINSKY, R. PALKO · AIAA Aerodynamic Testing Conference · 5

Semispan wind tunnel test of a computer-controlled self-optimizing flexible technology wing

1978 · E. LEVINSKY, R. PALKO · AIAA Aerodynamic Testing Conference · 5

Aerodynamic parameter optimization during wind tunnel testing

1982 · R. PALKO, M. CRAWFORD · AIAA Aerodynamic Testing Conference · 3

A constant aerodynamic parameter testing technique with automatic wind tunnel control

1978 · R. PALKO, A. LOHR · AIAA Aerodynamic Testing Conference · 3

A method of testing full-scale inlet/engine systems at high angles of attack and yaw at transonic velocities

1972 · R. PALKO · 8th Joint Propulsion Specialist Conference · 3

Initial Feasibility Ground Test of a Proposed Photogrammetric System for Measuring the Shapes of Ice Accretions on Helicopter Rotor Blades during Forward Flight

1984 · R. L. Palko, P. L. Cassady, et al. · 2

Photogrammetric development and application at AEDC

1982 · R. PALKO, P. CASSADY · AIAA Aerodynamic Testing Conference · 2

Full-scale inlet/engine testing at high maneuvering angles at transonic velocities

1972 · R. PALKO · AIAA Aerodynamic Testing Conference · 2

Supercritical tests of a self-optimizing, variable-Camber wind tunnel model

· Levinsky, E. S., Palko, R. L. · NASA Technical Reports Server (NASA) · 2

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Utilization of the AEDC three-dimensional potential flow computer program

1976 · R. PALKO · NASA Technical Reports Server (NASA) · 1

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Experimental Verification of a Technique for Testing Full-Scale Inlet/ Engine Systems at Angles of Attack up to 20 Deg at Transonic Speeds

1973 · R. L. Palko · 1

1-D Transient Thermal Modeling of an Ablative Material (MCC-1) Exposed to a Simulated Convective Titan 4 Launch Environment

1998 · Thomas R. Reinarts, William K. Crain, et al. · NASA STI Repository (National Aeronautics and Space Administration)

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Experimental Verification of an Aerodynamic Parameter Optimization Program for Wind Tunnel Testing

1981 · R. PALKO, M. CRAWFORD

The AEDC Three-Dimensional, Potential Flow Computer Program. Volume 2. Mathematical Modeling, Application, and Verification

1976 · R. PALKO

Aerodynamic Loads on Devices for Simulating Inlet/Engine Flow Conditions and Effects of Test Installation on Tunnel Operation

1975 · R. L. Palko

Experimental Verification of a Transonic Test Technique for Full-Scale Inlet/Engine Systems Simulating Maneuvering Attitudes

1974 · R. L. Palko

Development and experimental verification of a technique to test full-scale inlet/engine systems at maneuvering conditions

1974 · R. PALKO · AIAA/SAE/ASME/ASEE Joint Propulsion Conference (JPC)

Pressure distribution and flow visualization tests of a 1.5 elliptic cone at Mach 10 /

· Palko, R. L., author., Ray, A. D., author., et al. · University of Michigan Library Repository

The AEDC three-dimensional, potential flow computer program.

· Palko, Richard L., author., ARO, Inc. sponsor., et al. · University of Michigan Library Repository

Works count: 21

Citation count: 50

H-index: 4

I10-index: 1