Determination of longitudinal aerodynamic derivatives using flight data from an icing research aircraft
Author:
Affiliation:
1. NASA, Lewis Research Center, Cleveland, OH
2. NASA, Langley Research Center, Hampton, VA
3. NASA, Langley Research Center, Hampton, VA; George Washington University, Washington, DC
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1989-754
Reference21 articles.
1. Performance degradation of a typical twin engine commuter type aircraft in measured natural icing conditions
2. Icing flight research - Aerodynamic effects of ice and ice shape documentation with stereo photography
3. tion i n these derivatives, and this analysis was Y -5.66 -19.97
4. Mean value, Standard errors& Ratio, e -608 I ,0281 I ,0122 I 2.3 -1 .31 ,0147 ,0191 .a -34.2 ,6444 ,4314 1.5 -1.74 ,0248 ,0131 1.9
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