{"created": {"type": "/type/datetime", "value": "2009-12-11T03:22:05.859166"}, "title": "Further studies on the 21% thick, supercritical NLR airfoil NAE 68-060-21:1", "id": 45825817, "last_modified": {"type": "/type/datetime", "value": "2010-01-18T02:41:23.260581"}, "latest_revision": 2, "key": "/works/OL10656155W", "authors": [{"type": "/type/author_role", "author": {"key": "/authors/OL4441589A"}}], "type": {"key": "/type/work"}, "subjects": ["Reynolds number", "Drag", "Supersonic airfoils"], "revision": 2}