strip theory for oscillating thin wings with subsonic leading and supersonic trailing edges
By: Marten Landahl.
Contributors: U.S. Air Force. Office of Scientific Research
Series: OSR technical note -- no. 56-155; MIT Fluid Dynamics Research Group report -- no. 56-2
Publisher: Office of Scientific Research, United States Air Force
Published: 1956
Place of publication: [S.l.]
Number of pages: 19
Notes: Bibliographical references: p.14-15.

Contract number: AF18(600)-961