Navier-Stokes flowfield computation of wing/rotor interaction for a tilt rotor aircraft in hover
By: prepared for Ames Research Center.
Contributors: Ames Research Center
Publisher: Ames Research Center
Published: 1993
Place of publication: Washington, D. C
Number of pages: 142
Subjects: Hovering; Tilt rotor aircraft
Notes: Includes bibliographical references: p. 135-142.