Effects of roughness size on the position of boundary-layer transition and on the aerodynamic characteristics of a 55ê swept delta wing at supersonic speeds
By: Robert L. Stallings, Jr. and Milton Lamb
Contributors: Lamb, Milton, joint author; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office
Series: NASA technical paper ; 1027
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Office; for sale by the National Technical Information Service
Published: 1977
Place of publication: [Washington]; Springfield, Va
Language: eng
Number of pages: 47
Subjects: Boundary layer; Drag (Aerodynamics); Aerodynamics, Supersonic
Notes: Issued Dec. 1977

Includes bibliographical references