Any external aircraft modification has potentially far-reaching effects on the capability of the aircraft to succeed or fail in its mission. The authors take a systematic look at the effects that small changes can have upon the whole, with a series of examples that demonstrate why careful review of data or testing is often vital in the assessment of system modifications.
General Flight Test Theory Applied to Aircraft Modifications
1999
12 pages
Report
Keine Angabe
Englisch
Aerodynamics , Aerodynamic configurations , Flight testing , Modification , Design criteria , Requirements , Vibration , Stress analysis , Aircraft engines , Performance(Engineering) , Theory , Planning , External , Pressurization , Handling , Transport aircraft , Flutter , Airworthiness , C-130 aircraft
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