Publication Date:
2019-06-28
Description:
The equations used by the 16 foot transonic tunnel in the data reduction programs are presented in eight modules. Each module consists of equations necessary to achieve a specific purpose. These modules are categorized in the following groups: tunnel parameters; jet exhaust measurements; skin friction drag; balance loads and model attitudes calculations; internal drag (or exit-flow distributions); pressure coefficients and integrated forces; thrust removal options; and turboprop options. This document is a companion document to NASA TM-83186, A User's Guide to the Langley 16 Foot Transonic Tunnel, August 1981.
Keywords:
RESEARCH AND SUPPORT FACILITIES (AIR)
Type:
NASA-TM-86319-REV-1
,
NAS 1.15:86319-REV-1
Format:
application/pdf
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