{"created": {"type": "/type/datetime", "value": "2009-12-11T04:07:05.944427"}, "title": "High-Reynolds-number test of a 5-percent-thick low-aspect-ratio semispan wing in the Langley 0.3-meter transonic cryogenic tunnel, wing tunnel distributions", "id": 46318287, "last_modified": {"type": "/type/datetime", "value": "2010-01-19T18:36:43.493830"}, "latest_revision": 2, "key": "/works/OL11149116W", "authors": [{"type": "/type/author_role", "author": {"key": "/authors/OL4654358A"}}], "type": {"key": "/type/work"}, "subjects": ["Transonic wind tunnels", "Airplanes", "Wings"], "revision": 2}