Click here to make tpub.com your Home Page

Page Title: Center of Gravity (CG) Limitations
Back | Up | Next

Click here for thousands of PDF manuals

Google


Web
www.tpub.com

Home

   
Information Categories
.... Administration
Advancement
Aerographer
Automotive
Aviation
Construction
Diving
Draftsman
Engineering
Electronics
Food and Cooking
Logistics
Math
Medical
Music
Nuclear Fundamentals
Photography
Religion
   
   

 



Stability
T-45A/C TS, E2C2, ADV & IUT Aero-04
c.
Forward shift of center of pressure causing
pitch up
2.
Aerodynamic modifications to T-45 changed tip to
root stall characteristics
a.
3.5 degrees of geometric twist delays outboard
leading edge stall
b.
Stall strips enhance root stall to point that wing
tip stalls only slightly before root
c.
Stall strips induce airframe buffeting prior to
stall (1-2 knots clean, 1 knot dirty)
Sg 2, fr 13
M. Center of Gravity (CG) Limitations
Fig 5: Center of
Gravity Travel
1.
Point at which weight of an object can be considered
concentrated
2.
Aircraft designed for certain range of CG movement
3.
Factors affecting CG location in a tactical aircraft
Overlay 1
a.
landing gear position
Overlay 1
b.
fuel burned
c.
wing sweep
d.
ordnance
e.
ejection of aft seat
(9-99) Original
Page 4-9


Privacy Statement - Press Release - Copyright Information. - Contact Us

Integrated Publishing, Inc. - A (SDVOSB) Service Disabled Veteran Owned Small Business