An 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