Aerodynamic optimization studies using a 3-D supersonic Euler code with efficient calculation of sensitivity derivatives
Author:
Affiliation:
1. Old Dominion Univ., Norfolk, VA
2. NASA, Langley Research Center, Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1994-4270
Reference47 articles.
1. An approximately factored incremental strategy for calculating consistent discrete aerodynamic sensitivity derivatives
2. C Y m
3. +2.0925E-05 -1.2866 E-05 +6.1225 E-07 C M ,
4. +3.4438E-06 -5.7055E-06 -2.0632 E-06 &
5. +1.7229E-04 -7.6030E-05 -1.3698 E-05 (b) -SensitivityDerivative(SD) ratios, $:$-"$:% ( 3 OM Reduction)
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