<http://webisa.webdatacommons.org/prov/464330522>	<http://www.w3.org/ns/prov#wasDerivedFrom>	<http://webisa.webdatacommons.org/163925184> .
<http://webisa.webdatacommons.org/163925184>	<http://www.w3.org/ns/prov#value>	"FIG. 5B is an image illustrating a total field over a multi-element aircraft wing with flow control according to one embodiment of the present invention;" .
<http://webisa.webdatacommons.org/163925184>	<http://www.w3.org/1999/02/22-rdf-syntax-ns#type>	<http://www.w3.org/ns/prov#Entity> .
<http://webisa.webdatacommons.org/163925184>	<http://www.w3.org/ns/prov#wasQuotedFrom>	<google.com> .