Analytical procedure for computing smooth transitions between two specified cross sections with applications to blended wing-body configurations
By: Raymond L. Barger.
Contributors: Langley Research Center.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Series: NASA technical paper -- 2012.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1982
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 17
Subjects: Airplanes -- Wings.
Notes: "Langley Research Center."

"May 1982"--Cover.

Includes bibliographical references.