Influence of an Aft C. G. on Longitudinal Flying Qualities

720318

02/01/1972

Event
National Business Aircraft Meeting and Engineering Display
Authors Abstract
Content
The effects of aft center-of-gravity (cg) travel on the total longitudinal response characteristics of the aircraft are reviewed and the implications of this cg shift on the aircraft's longitudinal flying qualities discussed. In addition, variations in pitch damping, control gearing, and speed effects are discussed at specific aft cg locations. The examples used are based largely on experience gained during in-flight demonstration programs using the Cornell Aeronautical Laboratory, Inc. (CAL) variable stability B-26 aircraft.
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DOI
https://doi.org/10.4271/720318
Pages
16
Citation
Smith, R., "Influence of an Aft C. G. on Longitudinal Flying Qualities," SAE Technical Paper 720318, 1972, https://doi.org/10.4271/720318.
Additional Details
Publisher
Published
Feb 1, 1972
Product Code
720318
Content Type
Technical Paper
Language
English