Computation of Hinge-Moment Characteristics of Horizontal Tails from Section Data Page: 4 of 34
This report is part of the collection entitled: National Advisory Committee for Aeronautics Collection and was provided to Digital Library by the UNT Libraries Government Documents Department.
The following text was automatically extracted from the image on this page using optical character recognition software:
NACA CB No. 5B05
ol airfoil section lift coefficient --
L airfoil lift coefficient I
ch control-surface section hinge-moment coefficient
Oh elevator hinge-moment coefficient (.je)
Om airplane pitching-moment coefficient M )
t airfoil section lift
L airfoil lift
h control-surface section hinge moment
H elevator hinge moment
M airplane pitching moment about center of gravity
c chord of airfoil with control surface neutral, mean
geometric chord of horizontal tail
M.A.O. mean aerodynamic chord of wing
of chord of control surface aft of hinge line
ce mean geometric chord of elevator .aft of hinge line
ce root-mean-square chord of elevator aft of hinge line
Sw area of wing
Se area of elevator aft of hinge line
q dynamic pressure of air stream ( pV2)
In addition to these the following symbols have been
Here’s what’s next.
This report can be searched. Note: Results may vary based on the legibility of text within the document.
Tools / Downloads
Get a copy of this page or view the extracted text.
Citing and Sharing
Basic information for referencing this web page. We also provide extended guidance on usage rights, references, copying or embedding.
Reference the current page of this Report.
Crane, Robert M. Computation of Hinge-Moment Characteristics of Horizontal Tails from Section Data, report, April 1945; (digital.library.unt.edu/ark:/67531/metadc62480/m1/4/: accessed February 22, 2019), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.