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Jan Roskam

Jan Roskam (February 22, 1930 – September 9, 2022) was a Dutch-born American aircraft designer. He was the Deane E. Ackers Distinguished Professor of Aerospace Engineering at the University of Kansas. He was also the author of eleven books on airplane design and flight dynamics and over 160 papers on the topics of aircraft aerodynamics, performance, design and flight controls. He founded the company DARcorporation with Willem Anemaat. Provided by Wikipedia

Jan Roskam

Determination of the static performance of a Cuyuna 430 cc. model UL-430RR engine / by Roskam, Jan, 1930-

Weight and balance for the Airmass Incorporated Sunburst Model C ultralight / by Roskam, Jan, 1930-

Design, analysis and control of large transports so that control of engine thrust can be used as a back-up of the primary flight controls final technical report, grant #NAG 2-789 / by Roskam, Jan, 1930-

Determination of the static performance of a Cuyuna 430 cc. model UL-430RR engine / by Roskam, Jan, 1930-

Weight and balance for the Airmass Incorporated Sunburst Model C ultralight / by Roskam, Jan, 1930-

A parametric study of planform and aeroelastic effects on aerodynamic center, [alpha]- and q-stability derivatives : summary report / by Roskam, Jan, 1930-

Airplane flight dynamics and automatic flight controls / by Roskam, Jan, 1930-

Airplane design / by Roskam, Jan, 1930-

Airplane aerodynamics and performance / by Roskam, Jan, 1930-

An investigation into the vertical axis control power requirements for landing VTOL type aircraft onboard non-aviation ships in various sea states by Stevens, Mark E.

Jan Roskam

Determination of the static performance of a Cuyuna 430 cc. model UL-430RR engine / by Roskam, Jan, 1930-

Weight and balance for the Airmass Incorporated Sunburst Model C ultralight / by Roskam, Jan, 1930-

Design, analysis and control of large transports so that control of engine thrust can be used as a back-up of the primary flight controls final technical report, grant #NAG 2-789 / by Roskam, Jan, 1930-

Determination of the static performance of a Cuyuna 430 cc. model UL-430RR engine / by Roskam, Jan, 1930-

Weight and balance for the Airmass Incorporated Sunburst Model C ultralight / by Roskam, Jan, 1930-

A parametric study of planform and aeroelastic effects on aerodynamic center, [alpha]- and q-stability derivatives : summary report / by Roskam, Jan, 1930-

Airplane flight dynamics and automatic flight controls / by Roskam, Jan, 1930-

Airplane design / by Roskam, Jan, 1930-

Airplane aerodynamics and performance / by Roskam, Jan, 1930-

An investigation into the vertical axis control power requirements for landing VTOL type aircraft onboard non-aviation ships in various sea states by Stevens, Mark E.

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