Multi-Hole Pressure Probes to Air Data System for Subsonic Small-Scale Air Vehicles

被引：2

作者：

Shevchenko, A. M. ^{[1
]}

Berezin, D. R. ^{[2
]}

Puzirev, L. N. ^{[1
]}

Tarasov, A. Z. ^{[3
]}

Kharitonov, A. M. ^{[1
]}

Shmakov, A. S. ^{[1
]}

机构：

[1] Khristianovich Inst Theoret & Appl Mech SB RAS, Novosibirsk 630090, Russia

[2] Lutch JSC, Ribinsk 152920, Russia

[3] Sukhoi Co JSC, Moscow 125284, Russia

来源：

INTERNATIONAL CONFERENCE ON THE METHODS OF AEROPHYSICAL RESEARCH (ICMAR 2016) | 2016年 / 1770卷

基金：

俄罗斯基础研究基金会;

关键词：

D O I：

10.1063/1.4963947

中图分类号：

O59 [应用物理学];

学科分类号：

摘要：

A brief review of research performed to develop multi-hole probes to measure of aerodynamic angles, dynamic head, and static pressure of a flying vehicle. The basis of these works is the application a well-known classical multi hole pressure probe technique of measuring of a 3D flow to use in the air data system. Two multi-hole pressure probes with spherical and hemispherical head to air-data system for subsonic small-scale vehicles have been developed. A simple analytical probe model with separation of variables is proposed. The probes were calibrated in the wind tunnel, one of them is in-flight tested.

引用

页数：9

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