ISBN 9798676342531 is currently unpriced. Please contact us for pricing.
Available options are listed below:
Available options are listed below:
Data Reduction Functions for the Langley 14- by 22-Foot Subsonic Tunnel
| AUTHOR | Administration (Nasa), National Aeronaut |
| PUBLISHER | Independently Published (08/21/2020) |
| PRODUCT TYPE | Paperback (Paperback) |
Description
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
Show More
Product Format
Product Details
ISBN-13:
9798676342531
Binding:
Paperback or Softback (Trade Paperback (Us))
Content Language:
English
More Product Details
Page Count:
78
Carton Quantity:
52
Product Dimensions:
8.50 x 0.16 x 11.02 inches
Weight:
0.45 pound(s)
Country of Origin:
US
Subject Information
BISAC Categories
Reference | Research
Reference | Space Science - General
Descriptions, Reviews, Etc.
publisher marketing
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
Show More