Summary The thermal insulation system of the Langley 0.3- Meter Transonic Cryogenic Tunnel is described. ... The time required for opening and closing portions of the insulation system for modification or repair to the tunnel has been reduced, typically, from a few days for the original ... a particular flight or fluid flow regime.
|Title||:||Description of the insulation system for the Langley 0.3-meter transonic cryogenic tunnel|
|Author||:||Pierce L. Lawing, David A. Dress, Robert A. Kilgore, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch|