Research Catalog

Low-speed aerodynamic characteristics of a wing-canard configuration with underwing spanwise blowing on the trailing-edge flap system

Title
Low-speed aerodynamic characteristics of a wing-canard configuration with underwing spanwise blowing on the trailing-edge flap system [microform] / Daniel W. Banks and John W. Paulson.
Author
Banks, Daniel W.
Publication
[Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : National Technical Information Service, distributor], 1987.

Details

Additional Authors
  • Paulson, John W.
  • United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.
Description
1 v.
Series Statement
NASA technical memorandum ; 89020
Alternative Title
Low speed aerodynamic characteristics of a wing canard configuration with underwing spanwise blowing on the trailing edge flap system
Subject
  • Aerodynamic characteristics
  • Canard configurations
  • Low speed
  • Spanwise blowing
  • Trailing edge flaps
Note
  • Distributed to depository libraries in microfiche.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.15:89020
OCLC
marcive33001237
Author
Banks, Daniel W.
Title
Low-speed aerodynamic characteristics of a wing-canard configuration with underwing spanwise blowing on the trailing-edge flap system [microform] / Daniel W. Banks and John W. Paulson.
Imprint
[Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : National Technical Information Service, distributor], 1987.
Series
NASA technical memorandum ; 89020
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1987] a microfiche.
Added Author
Paulson, John W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.
Gpo Item No.
0830-D (MF)
Sudoc No.
NAS 1.15:89020
Research Call Number
READEX Microfiche NAS 1.15:89020
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