Advanced Topics in Aerodynamics, Aerodynamic Database (AD)
http://aerodyn.org/HighLift/tables.html
---
CLmax			3.45	(in ground effect)



Butterworth-Heinemann
http://www.bh.com/companions/034074152X/appendices/data-a/table-8/table.htm
---
CLmax (t/o)		2.17	(Df = 15 degrees)
CLmax (l/d@MLM)		2.59	(Df = 42 degrees)




Lissys
http://www.lissys.demon.co.uk/f7tx2.html
(Note: Simulated Fokker 70 data)
---
CLmax (t/o)		1.91	(Df =  0 degrees)
L/D (2nd sgement)	12.54	(incl. windmill. & asymm).

CLmax (l/d)		2.43	(Df = 42 degrees)
L/D (approach)		4.91	(gear down)


CD0	0.01922
CDi	0.00867
CDM	0.00115
CDtrim	0.00013

L/D	15.08
TSFC	0.6908



http://www.aoe.vt.edu/~mason/Mason_f/CAtxtChap5.pdf
(Data for the DC-9)
(Note that the design limmit of the Fokker 100 is set at M0.88)
---
CDm

MACH	CDmach
0	0
0.6	0
0.78	0.018
0.79	0.020
0.81	0.039



Add a description about the data used.
Add a description about the data used.
