Research Catalog

A semiempirical method for obtaining fuselage normal areas from fuselage mach sliced areas

Title
A semiempirical method for obtaining fuselage normal areas from fuselage mach sliced areas [microform] / Robert J. Mack, Kathy E. Needleman.
Author
Mack, Robert J.
Publication
[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : National Technical Information Service, distributor], 1990.

Details

Additional Authors
  • Needleman, Kathy E.
  • United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.
Description
1 v.
Series Statement
NASA technical memorandum ; 4228
Subject
  • Aircraft configurations
  • Aircraft design
  • Force distribution
  • Fuselages
  • Mach number
  • Sonic booms
Note
  • Distributed to depository libraries in microfiche.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.15:4228
OCLC
marcive32384407
Author
Mack, Robert J.
Title
A semiempirical method for obtaining fuselage normal areas from fuselage mach sliced areas [microform] / Robert J. Mack, Kathy E. Needleman.
Imprint
[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : National Technical Information Service, distributor], 1990.
Series
NASA technical memorandum ; 4228
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1991] 2 microfiches.
Added Author
Needleman, Kathy E.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.
Gpo Item No.
0830-D (MF)
Sudoc No.
NAS 1.15:4228
Research Call Number
READEX Microfiche NAS 1.15:4228
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