Control Hinge-Moment and Effectiveness Characteristics of a 60 Degree Half-Delta Tip Control on a 60 Degree Delta Wing at Mach Numbers of 1.41 and 1.96 Page: 4 of 41
This report is part of the collection entitled: National Advisory Committee for Aeronautics Collection and was provided to UNT Digital Library by the UNT Libraries Government Documents Department.
Extracted Text
The following text was automatically extracted from the image on this page using optical character recognition software:
NACA RM L52H13
Cm
gross
CBMf
Ch
C ,ACL,ACm
q
S
Sf
c
f
b
bf
8sav
Pitching moment
pitching-moment coefficient, ; pitching-
qS~
moment reference axis located at 0.25C
gross rolling-moment coefficient,
Semispan wing rolling moment
2qSb ; reference axis shown in
2qSb
figure 1
control bending-moment coefficient, Bending moment.
qSfbf
reference axis is root chord of control surface
Hinge moment
control hinge-moment coefficient, ; reference
qSfcf
axis is hinge line
increment in gross rolling-moment coefficient, lift
coefficient, and pitching-moment coefficient due to
deflection of the control surface
free-stream dynamic pressure
semispan wing area (including area blanketed by fuselage)
control-surface area
local wing chord
mean aerodynamic chord of wing
mean aerodynamic chord of control surface
wing span (twice distance from rolling-moment reference
axis to wing tip)
control-surface span (distance from parting line to tip)
angle of attack measured with respect to free stream
control-surface deflection measured with respect to wing-
chord plane.
average control-surface deflectioni-aa
Upcoming Pages
Here’s what’s next.
Search Inside
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.
Guy, Lawrence D. Control Hinge-Moment and Effectiveness Characteristics of a 60 Degree Half-Delta Tip Control on a 60 Degree Delta Wing at Mach Numbers of 1.41 and 1.96, report, October 14, 1952; (https://digital.library.unt.edu/ark:/67531/metadc59409/m1/4/?rotate=270: accessed April 24, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.