Aerodynamic characteristics at Mach numbers of 1.5, 1.8, and 2.0 of a blended wing-body configuration with and without integral canards
By: A. Warner Robins, Milton Lamb, and David S. Miller, Langley Research Center
Contributors: Lamb, Milton, joint author; Miller, D. S. joint author; Langley Research Center; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office
Series: NASA technical paper ; 1427
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Office; for sale by the National Technical Information Office
Published: 1979
Place of publication: [Washington]; Springfield, Va
Language: eng
Number of pages: 56
Subjects: Hypersonic planes; Stability of airplanes
Notes: May 1979

Includes bibliographical references