A semiempirical method for obtaining fuselage normal areas from fuselage mach sliced areas
By: Robert J. Mack, Kathy E. Needleman.
Contributors: Needleman, Kathy E.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.
Series: NASA technical memorandum -- 4228.
Publisher: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division; National Technical Information Service, distributor]
Published: 1990
Place of publication: [Washington, DC]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Aircraft configurations.; Aircraft design.; Force distribution.; Fuselages.; Mach number.; Sonic booms.
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1991] 2 microfiches.