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

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Smith, Rogers E., author.
Conference Name:
National Business Aircraft Meeting and Engineering Display (1972-03-15 : Wichita, Kansas, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1972
Summary:
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, Incorporated (CAL) variable stability B-26 aircraft
Notes:
Vendor supplied data
Publisher Number:
720318
Access Restriction:
Restricted for use by site license

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