effect of pitch and yaw on the aerodynamic interference between two identical, unstaggered, axisymmetrical bodies whose centrelines are parallel and separated by 1.11 body diameters
By: D. I. T. P. Llewelyn-Davies.
Contributors: Cranfield Institute of Technology. College of Aeronautics
Series: Cranfield College of Aeronautics report -- no. 8909
Publisher: Cranfield Institute of Technology, College of Aeronautics
Published: 1989
Place of publication: Cranfield, Bedford, England
Subjects: Aerodynamic interference; Pitch; Yaw
Notes: Includes bibliographical references.