PRESSURE FIELDS INVESTIGATION BY LPS TECHNOLOGY ON THE AEROSPACECRAFTMODEL

Authors
ANDREEV AO BUKOV AP IPATOV MW KABIN SV NUSHTAEV PD ORLOV AA MOSHAROV VE RADCHENKO VN PESETSKY VK PHONOV SD
Citation
Ao. Andreev et al., PRESSURE FIELDS INVESTIGATION BY LPS TECHNOLOGY ON THE AEROSPACECRAFTMODEL, Journal de physique. III, 4(11), 1994, pp. 2317-2327
Citations number
14
Categorie Soggetti
Material Science","Phsycs, Fluid & Plasmas","Physics, Applied
Journal title
Journal de physique. III → ACNP
ISSN journal
11554320
Volume
4
Issue
11
Year of publication
1994
Pages
2317 - 2327
Database
ISI
SICI code
1155-4320(1994)4:11<2317:PFIBLT>2.0.ZU;2-N
Abstract
The results of Luminescence Pressure Sensor (LPS) technology applicati ons for pressure field measurements on the surface of aerospacecraft m odel ''BURAN'' are presented. Physical principles of LPS technology, a n experimental technique and data reduction method are considered. A f low around model was investigated at Mach number range 0.85 divided-by 0.96 and angles of attack range 8-degrees divided-by 16-degrees.