# Movable trailing edge flaps implementation

**URL:** <https://forums.nlr.gov/t/movable-trailing-edge-flaps-implementation/858>\
**Category:** Rotor Aerodynamics\
**Created:** [March 12, 2014, 1:50pm UTC](https://forums.nlr.gov/t/movable-trailing-edge-flaps-implementation/858 "2014-03-12T13:50:21Z")\
**Posts on this page:** 1\
**Showing post:** 36

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**Author:** ![Jason.Jonkman](https://dub1.discourse-cdn.com/nrel/user_avatar/forums.nlr.gov/jason.jonkman/32/3086_2.png) [@Jason.Jonkman](https://forums.nlr.gov/u/Jason.Jonkman)\
**Post date:** [September 21, 2016, 1:44pm UTC](https://forums.nlr.gov/t/movable-trailing-edge-flaps-implementation/858/36 "2016-09-21T13:44:27Z")

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Dear Srinivasa,

Regarding the airfoil geometry of the NREL 5-MW baseline turbine, please see my post dated Jun 04, 2012 in the following forum topic: [NREL 5MW Rotor Geometry - #4 by Kisorthman.Vimalakan](http://forums.nlr.gov/t/nrel-5mw-rotor-geometry/330/4).

Best regards,

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