Theoretical stability derivatives of a highly swept delta wing and slender body combination
By: T. Nonweiler.
Contributors: College of Aeronautics (Cranfield, Bedfordshire)
Series: College of Aeronautics -- Cranfield. Report ; no. 50
Publisher: College of Aeronautics
Published: 1951
Place of publication: Cranfield, Bedfordshire
Number of pages: 36
Notes: Bibliographical references: p. 27.