Wind-tunnel measurements of air loads on split flaps /
Saved in:
Main Author: | Wenzinger, Carl J. 1903-1988 (Author) |
---|---|
Format: | Government Document Electronic eBook |
Language: | English |
Published: |
Washington, [D.C.] :
National Advisory Committee for Aeronautics,
1934.
|
Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
498. |
Subjects: | |
Online Access: | CONNECT |
Similar Items
-
The aerodynamic characteristics of a model wing having a split flap deflected downward and moved to the rear /
by: Weick, Fred E., et al.
Published: (1932) -
Full-scale span load distribution on a tapered wing with split flaps of various spans /
by: Parsons, John F., et al.
Published: (1937) -
Pressure distribution over a Clark Y-H airfoil section with a split flap /
by: Wenzinger, Carl J. 1903-1988
Published: (1937) -
Wind-tunnel tests of a Clark Y wing having split flaps with gaps /
by: Wenzinger, Carl J. 1903-1988
Published: (1938) -
The effects of full-span and partial-span split flaps on the aerodynamic characteristics of a tapered wing /
by: Wenzinger, Carl J. 1903-1988
Published: (1934)