Data Reduction Functions for the Langley 14- by 22-Foot Subsonic Tunnel

By: Administration (Nasa), National Aeronaut

The Langley 14- by 22-Foot Subsonic Tunnel's data reduction software utilizes six major functions to compute the acquired data. These functions calculate engineering units, tunnel parameters, flowmeters, jet exhaust measurements, balance loads/model attitudes, and model /wall pressures. The input (required) variables, the output (computed) variables, and the equations and/or subfunction(s) associated with each major function are discussed. Boney, Andy D. Langley Research Center NASA/TM-2014-218513, L-19877, NF1676L-10710 WBS 122711.03.07.07.05.80

• Format: Paperback
• Language: English
• ISBN: B08GDK9L4C
• ISBN13: 9798676342531
• Release Date: January 1
• Publisher: Independently Published
• Length: 78 Pages
• Weight: 0.45 lbs.
• Dimensions: 0.2" x 8.5" x 11.0"