theoretical wave drag at zero lift of fully-tapered swept wings of arbitrary section
By: T. Nonweiler.
Contributors: College of Aeronautics (Cranfield, Bedfordshire)
Series: College of Aeronautics -- Cranfield. Report ; no. 76
Publisher: College of Aeronautics
Published: 1953
Place of publication: Cranfield, Bedfordshire
Number of pages: 42
Notes: Bibliographical references: p. 23.