AEG EFK 61 User Manual Page 2

  • Download
  • Add to my manuals
  • Print
  • Page
    / 76
  • Table of contents
  • BOOKMARKS
  • Rated. / 5. Based on customer reviews
Page view 1
__. _.—.. —__ .——.—-
TEQH LIBRARY
KAFB,NM
IN
m!rIoNAL ADvmoRY cOmITIEm
~
Illfllllllllloll!ulluo
FOR AERONAUTICS
011b57~b
TECHNICAL NOTE
MEAS~ OF FLYING QUALITIES
2899
OF JUTF-471)-30AXWMIE
TO DETERMINE LONGITUDINAL”STABILITY AND CONTROL
AND STALLING CHARACTERISTIC~
By Christopher C. Kraft, Jr., R. Fabian Goranson,
and John P. Reeder
t
Flight tests have been made -to determine the longitudinal stabili~
and control and stalling cbacteristics of m F-47D-30 airplane. The
results of these tests show the airplane to be unstible with stick free
in any power-on condition even at the most forward center-of-gravi@
position tested: At the re
arward center-of-gravityposition tested the
airplane also had neutral to negative stick-fixed stabili~ with power
on. The characteristics in accelerated flight were acceptdle at the
forward center-of-gravityposition at low and high altitudes except at
high speed where the control-force variations with acceleration were
high.
At the rearwsrd center-of-gravityposition, elevator-force rever-
sals were experienced in turns at low speeds, and the elevator-force
variations with acceleration were low at all the other speeds tested.
Ample stall warning was afforded in all the conditions tested and the
stalling characteristics were satisfactory except in the approach and
wave-off conditions.
&
Introduction
This paper presents an investigation of the flying qualities of the
F-47D-30 airplane.
Many flying-qualities investigations have been con-
ducted by the National Advisory Comittee for Aeronautics with vario~
types of airplanes and this paper is intended to supplement this infor-
mation.
By correction of these da~a with pilot opinions of these ati-
phes, it has been possible to establish quantitative re@rements for
satisfactory flying qualities such as those presented in reference 1.
%.qersedes therecently declassified NACARMS~A06 for the Air
Materiel Command, ArIW Air Forces, “Flight Measurements of Flying Qml-
ities of a P-47D-30 Airplane (AAF No. 43-34-41)to Determine Longitudinal’
r-?
Stability and Control and Stalling Characteristics” by Christopher C.
I&aft, Jr.,
R. Fabian Goranson, and John P. Reeder, 1948.
. . —.— —-..-——------ —-—--- -..------————---
.—. ---- ---- -.——- —-——
--—” -.—-—— --- --
Page view 1
1 2 3 4 5 6 7 ... 75 76

Comments to this Manuals

No comments