<http://webisa.webdatacommons.org/prov/465072137>	<http://www.w3.org/ns/prov#wasDerivedFrom>	<http://webisa.webdatacommons.org/174894859> .
<http://webisa.webdatacommons.org/prov/464780395>	<http://www.w3.org/ns/prov#wasDerivedFrom>	<http://webisa.webdatacommons.org/174894859> .
<http://webisa.webdatacommons.org/174894859>	<http://www.w3.org/ns/prov#value>	"FIGS. 8A, 8B and 8C are a flow chart illustrating the application of a response surface methodology (RSM) used in this invention to obtain an optimal cross-sectional shape of an airfoil, as an example, where specified pressure values at selected locations on the airfoil perimeter are to be matched as closely as possible." .
<http://webisa.webdatacommons.org/prov/464323334>	<http://www.w3.org/ns/prov#wasDerivedFrom>	<http://webisa.webdatacommons.org/174894859> .
<http://webisa.webdatacommons.org/174894859>	<http://www.w3.org/ns/prov#wasQuotedFrom>	<google.com> .
<http://webisa.webdatacommons.org/174894859>	<http://www.w3.org/1999/02/22-rdf-syntax-ns#type>	<http://www.w3.org/ns/prov#Entity> .