Index of /drela/Public/web/hpa/airfoils

      Name                    Last modified       Size  Description


[DIR] Parent Directory        31-Oct-2020 00:08      -  
[   ] dae11.dat               20-Sep-2007 13:05     4k  
[   ] dae21.dat               20-Sep-2007 13:06     2k  
[   ] dae31.dat               20-Sep-2007 13:06     2k  
[   ] dae41.dat               20-Sep-2007 13:06     2k  
[   ] dae51.dat               20-Sep-2007 13:06     2k  
[   ] dai0735.dat             07-Mar-2012 11:14     2k  
[   ] dai1238.dat             20-Sep-2007 13:07     2k  
[   ] dai1335.dat             20-Sep-2007 13:07     2k  
[   ] dai1336.dat             20-Sep-2007 13:06     2k  
[   ] gw19.dat                30-May-2020 12:00     6k  
[   ] gw25.dat                30-May-2020 12:00     6k  
[   ] gw27.dat                30-May-2020 12:01     6k  
[   ] gw30.dat                30-May-2020 12:01     6k  
[   ] gw31.dat                30-May-2020 15:07     6k  
[   ] mrc12.dat               07-Apr-2016 17:55     2k  
[   ] mrc15.dat               24-Apr-2010 11:56     3k  
[   ] mrc16-85.dat            07-Apr-2016 17:56     3k  
[   ] mrc16-95.dat            07-Apr-2016 17:56     3k  
[   ] mrc16.dat               24-Apr-2010 11:55     3k  
[   ] mrc20-700.dat           07-Apr-2016 17:56     3k  
[   ] mrc20-846.dat           07-Apr-2016 17:57     3k  
[   ] mrc20.dat               07-Apr-2016 17:56     3k  


Human-powered aircraft and hydrofoil airfoils

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Daedalus

dae11.dat    center panel, mid-panel inner end  ;  design  Re=500K
dae21.dat    mid-panel outer end                ;  design  Re=375K
dae31.dat    tip panel, 4.5 ft (1.4 m) from tip ;  design  Re=250K
dae41.dat    wingtip                            ;  design  Re=150K
dae51.dat    propeller                          ;  design  Re=150K

-----------------------------------------------------
Light Eagle

dai1335.dat  center panel, mid-panel inner end 
dai1336.dat  mid-panel outer end	       
dai1238.dat  tip 

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Decavitator

mrc12.dat      v.1 takeoff and  high-speed wings  ; design  Re=300K
mrc15.dat      front stabilizers, all versions    ; design  Re=150K

mrc16.dat      v.2 takeoff wing center            ; design  Re*sqrt(CL)=250K
mrc16-95.dat   v.2 takeoff wing 80% semispan      ; design  Re*sqrt(CL)=200K
mrc16-85.dat   v.2 takeoff wing tip               ; design  Re*sqrt(CL)=175K

mrc20.dat      v.2 high-speed wing center         ; design  Re=350K
mrc20-846.dat  v.2 high-speed wing 80% semispan
mrc20-700.dat  v.2 high-speed wing tip

-----------------------------------------------------
Leading Systems / General Atomics  Gnat, Predator A

Flap hinge at x/c=0.75
max -15deg deflection for dash config

gw19.dat   P root         ;  design Re*sqrt(CL)=1500K
gw25.dat   P tip, G root  ;  design Re*sqrt(CL)=600K
gw27.dat          G tip   ;  design Re*sqrt(CL)=300K