Kenneth P. Spreemann

Investigation of the Effectiveness of Boundary-layer Control by Blowing over a Combination of Sliding and Plain Flaps in Deflecting a Propeller Slipstream Downward for Vertical Take-off

Richard E. Kuhn, Kenneth P. Spreemann, 1956 .

Aerodynamic characteristics of a wing with quarter-chord line swept back 45 degrees, aspect ratio 6, taper ratio 0.6, and NACA 65A009 airfoil section

Kenneth P. Spreemann, William D. Morrison, Thomas B. Pasteur, 1949 .

Preliminary Investigation of the Static Longitudinal and Lateral Stability Characteristics of a 0.05-Scale Model of the Convair F2Y-1 Airplane at High Subsonic Speeds

Kenneth P. Spreemann, Albert G. Few, 1954 .

Preliminary Investigation of the Effectiveness of a Sliding Flap in Deflecting a Propeller Slipstream Downward for Vertical Take-off

Richard E. Kuhn, Kenneth P. Spreemann, 1956 .

Investigation of Interference of a Deflected Jet with Free Stream and Ground on Aerodynamic Characteristics of a Semispan Delta-Wing VTOL Model

Kenneth P. Spreemann, K. Spreemann, 1961 .

Design Guide for Pitch-Up Evaluation and Investigation at High Subsonic Speeds of Possible Limitations Due to Wing-Aspect-Ratio Variations

Kenneth P. Spreemann, 1959 .