Author

David R. Clark

Observed names: D. R. Clark, David Clark

Observed institutions: Sikorsky Aircraft Corporation (United States), United Technologies (United States)

OpenAlex ID: A5109379092

THE FREE WAKE ANALYSIS: A method for the prediction of helicopter rotor hovering performance.

1969 · David R. Clark, Albert C. Leiper · Vertical Flight Society Forum · 44

The Free Wake Analysis

1970 · David R. Clark, Albert C. Leiper · Journal of the American Helicopter Society · 38

Aerodynamic Technology for Advanced Rotorcraft‐Part I

1977 · Anton J. Landgrebe, Robert C. Moffitt, et al. · Journal of the American Helicopter Society · 35

A Method for Predicting Helicopter Hub Drag

1976 · Thomas W. Sheehy, David R. Clark · Defense Technical Information Center (DTIC) · 18

Lifting Surface Method For Hover/Climb Airloads

1979 · David R. Clark · 13

Study for prediction of rotor/wake/fuselage interference, part 1

1985 · David R. Clark, B. Maskew · NASA STI Repository (National Aeronautics and Space Administration) · 10

PDF

Wind Tunnel Tests of Large- and Small-Scale Rotor Hubs and Pylons

1981 · A. H. Logan, Raymond W. Prouty, et al. · 5

Aerodynamic Technology for Advanced Rotorcraft—Part II

1977 · Anton J. Landgrebe, Robert C. Moffitt, et al. · Journal of the American Helicopter Society · 5

Aerodynamic Design Rationale For The Fan-In-Fin On The S-67 Helicopter

1975 · David R. Clark · Vertical Flight Society Forum · 5

Calculation of rotor/airframe interference for realistic configurations

1982 · David R. Clark, B. Maskew · NASA Technical Reports Server (NASA) · 4

Can Helicopter Rotors Be Designed For Low Noise And High Performance?

1974 · David R. Clark · Vertical Flight Society Forum · 4

Analysis Of The Wing/Rotor And Rotor/Rotor Interactions Present In Tilt-Rotor Aircraft

1985 · David Clark · AHS Specialists Meeting on Rotorcraft Basic Research · 1

A Lifting-Surface Method for Hover/Climb Airloads

1979 · J. Michael Summa, David R. Clark · Vertical Flight Society Forum · 1

On the flow in the nozzle of a condensing diatomic vapour

1963 · David R. Clark · College of Aeronautics Report · 1

Use of Computer Models In Helicopter Drag Prediction

1987 · David Clark, Brian Maskew · AHS Specialists Meeting on Aerodynamics and Aeroacoustics

Study for prediction of rotor/wake/fuselage interference. Part 2: Program users guide

1985 · David R. Clark, B. Maskew · NASA STI Repository (National Aeronautics and Space Administration)

PDF

Application of an Aerodynamic Configuration Modeling Technique to the Design and Analysis of X‐Wing Aircraft Configurations

1981 · D. R. Clark, R. T. Leitner · Journal of the American Helicopter Society

Development of Aerodynamic Modelling Methods to Include Separated Flow

1980 · David R. Clark · Journal of the American Helicopter Society

The Experimental and Analytical Definition of Helicopter Modeling Effects

1980 · David R. Clark, Andrew H. Logan, et al. · Vertical Flight Society Forum

Integrated Analytical And Experimental Investigation Of Helicopter Hub Drag

1979 · A. H. Logan, R. Marthe, et al.

An Integrated Analytical and Experimental Investigation of Helicopter Hub Drag

1979 · David R. Clark, Andrew H. Logan, et al. · Vertical Flight Society Forum

Rotor blade boundary layer measurement hardware feasibility demonstration

1972 · David R. Clark, T. D. Lawton · NASA STI Repository (National Aeronautics and Space Administration)

PDF

The Cranfield helium hypersonic wind tunnel: Tunnel, plant and instrumentation

1965 · David R. Clark · College of Aeronautics Report

Works count: 23

Citation count: 184

H-index: 6

I10-index: 6