NASA Common Research Model

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Aerodynamic and Icing Conditions

Flight Reference Values

IRT Test Conditions Run Log:

- Inboard
- Midspan
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HIGH LIFT CRM

High Lift CRM installed in the 14x22 foot subsonic tunnel at NASA Langley Research Center

CRM WITH NATURAL LAMINAR FLOW WING

Common Research Model with Natural Laminar Flow wing installed in the National Transonic Facility at NASA Langley Research Center.

ICING RESEARCH TUNNEL CRM

portion of the Common Research Model wing installed in the Icing Research Tunnel at NASA Glenn Research Center

NASA Responsible Official: Melissa Rivers

Page Curator: Melissa Rivers

Page Last Modified: April 1, 2022

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