Dynamic Pressure Equations Used at the 14- by 22-Foot Subsonic Tunnel

Quinto, P Frank ; Boney, Andy D

关键词: DYNAMIC PRESSURE;    SUBSONIC WIND TUNNELS;    TEST CHAMBERS;    DYNAMICS;    KINETIC THEORY;   

RP-ID  :  NF1676L-32662

学科分类：航空航天科学

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来源: NASA Technical Reports Server

【 摘 要 】

This document provides a description of equations used to calculate test section dynamic pressure in the 14- by 22-Foot Subsonic Tunnel. The equation used to calculate dynamic pressure is dependent on the test section configuration.