Richard E Kuhn

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Aerodynamic Characteristics in Pitch and Sideslip at High Subsonic Speeds of a 1/14-Scale Model of the Grumman XF104 Airplane with Wing Sweepback of 42.5 Degrees

Richard E Kuhn, John W Draper, 1953 .

An Engineering Method for Estimating the Lateral/Directional Characteristics of V/STOL Configurations in Transition.

Richard E Kuhn, 1981 .

An Examination of the Factors Affecting the Thrust Requirements and the Hover and Short Takeoff Performance of Several Jet V/STOL Fighter Concepts,

Richard E Kuhn, 1978 .

High Pressure Bleed for STOL and STO-VL Performance - A Conceptual Examination.

Richard E Kuhn, 1982 .

Investigation at Zero Forward Speed of a Leading-edge Slat as a Longitudinal Control Device for Vertically Rising Airplanes that Utilize the Redirected-slipstream Principle

Richard E Kuhn, R. Kuhn, 1956 .

Investigation of effectiveness of large-chord slotted flaps in deflecting propeller slipstreams downward for vertical take-off and low-speed flight

Richard E Kuhn, John W Draper, R. Kuhn, 1955 .

An Engineering Method for Estimating the Induced Lift on V/STOL Aircraft Hovering in and Out of Ground Effect.

Richard E Kuhn, 1981 .

On the Prediction of the Lateral/Directional Characteristics of Distributed Jet STOL Configurations.

Richard E Kuhn, 1982 .

Investigation of the effects of ground proximity and propeller position on the effectiveness of a wing with large-chord slotted flaps in redirecting propeller slipstreams downward for vertical take-off

Richard E Kuhn, R. Kuhn, 1956 .

Research and Development Needs of Vertical Attitude Takeoff and Landing (VATOL) Aircraft

Richard E Kuhn, 1979 .

The effect of tip tanks on the rolling characteristics at high subsonic Mach numbers of a wing having an aspect ratio of 3 with quarter-chord line swept back 35 degrees

Richard E Kuhn, Boyd C Myers, 1950 .

Conceptual Study of Modifying an Existing Fighter for V/STOL Capability and Combat Maneuvering Enhancement.

Richard E Kuhn, 1980 .

Investigation of Effectiveness of a Wing Equipped with a 50-percent-chord Sliding Flap, a 30-percent-chord Slotted Flap, and a 30-percent-chord Slat in Deflecting Propeller Slipstreams Downward for Vertical Take-off

Richard E Kuhn, 1957 .

Height of Spray Produced by Vertical Takeoff and Landing (VTOL) Aircraft

Richard E Kuhn, 1979 .

Investigation of the aerodynamic characteristics of a model wing-propeller combination and of the wing and propeller separately at angles of attack up to 90 degrees

Richard E Kuhn, John W Draper, R. Kuhn, 1956 .

Prediction of Drag Coefficients of a Supersonic V/STOL Configuration with Various Store Arrangements,

Richard E Kuhn, Thomas H Boyd, Tsze C Tai, 1979 .

An investigation of a wing-propeller configuration employing large-chord plain flaps and large-diameter propellers for low-speed flight and vertical take-off

Richard E Kuhn, R. Kuhn, J. Draper, 1954 .

Wind-tunnel Investigation of Effect of Propeller Slipstreams on Aerodynamic Characteristics of a Wing Equipped with a 50-percent-chord Sliding Flap and a 30-percent-chord Slotted Flap

Richard E Kuhn, W. C. Hayes, William C Hayes, 1957 .