Effects of configuration geometry on the transonic aerodynamic characteristics of canard airplane configurations /
Saved in:
Main Author: | Blackwell, James A., Jr |
---|---|
Corporate Authors: | United States National Aeronautics and Space Administration, Langley Research Center |
Other Authors: | Kelly, Thomas C |
Format: | Book |
Language: | English |
Published: |
Washington, D.C. :
National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia],
1964
|
Series: | NASA technical note ;
D-2465 NASA technical note ; D-2465 |
Subjects: | |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Effect of canard location and size on canard-wing interference and aerodynamic-center shift related to maneuvering aircraft at transonic speeds /
by: Gloss, Blair B
Published: (1974) -
Hypersonic aerodynamic characteristics of aircraft configurations with canard controls /
by: Brooks, Cuyler W, et al.
Published: (1966) -
Effect of canard leading-edge sweep and dihedral angle on the longitudinal and lateral aerodynamic characteristics of a close-coupled canard-wing configuration /
by: Gloss, Blair B
Published: (1974) -
Wind-tunnel investigation of the flight characteristics of a Canard general-aviation airplane configuration
by: Satran, Dale R
Published: (1986) -
High angle canard missile test in the Ames 11-foot transonic wind tunnel /
by: Schwind, Richard G
Published: (1978)