Further investigation of a finite difference procedure for analyzing the transonic flow about harmonically oscillating airfoils and wings
By: W. H. Wetherill ... [et al.] ; prepared for Langley Research Center under contract NAS1-15128
Contributors: Weatherill, W. H; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office; Langley Research Center
Series: NASA contractor report -- 3195
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Office; For sale by the National Technical Information Service]
Published: 1980
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 79
Subjects: Aerodynamics, Transonic
Notes: "May 1980"--Cover

STAR category no. 02

Includes bibliographical references