Numerical simulation and comparison of symmetrical/supercritical airfoils for the near tip region of a helicopter in forward flight
By: prepared for Langley Research Center.
Contributors: Langley Research Center; Planning Research Corporation. Aerospace Technologies Division
Publisher: Langley Research Center
Published: 1989
Place of publication: Hampton, Va
Number of pages: 51
Subjects: Aerodynamic loads; Helicopters; Rotary wings
Notes: Bibliographical references: p.24.