Volume 4; Issue 1

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Volume 4; Issue 1

Aircraft Design

Letter to the Editor: Range and endurance of turboprop, turbofan, or piston-propeller aircraft having wings with or without camber (Ref. 3)

Design of low-speed aircraft by numerical and experimental techniques developed at DPA

On-line parameter estimation for restructurable flight control systems

Mass distribution management & dynamic balancing of aircraft mass

Preliminary aircraft design: lateral handling qualities

Aircraft performance, theory and practice: M.E. Eshelby; Arnold Engineering, London, 2000, 288p. ISBN 0&#xa0;340&#xa0;75897 X; Also published in the AIAA Education Series, Washington, 2000, ISBN 1-56347-398-4.

Aircraft performance, theory and practice: M.E. Eshelby; Arnold Engineering, London, 2000, 288p. ISBN 0 340 75897 X; Also published in the AIAA Education Series, Washington, 2000, ISBN 1-56347-398-4.