Wing flow tests at subsonic and transonic speeds on four thin, low aspect ratio, swept-back wings
By: A. D. Wood and D. H. Henshaw.
Contributors: Henshaw, D. H.; National Aeronautical Establishment (Canada)
Series: National Aeronautical Establishment. Laboratory report -- LR-118
Publisher: National Aeronautical Establishment
Published: 1954
Place of publication: Ottawa