electronic library
metadata only
Investigation of shock-induced flow separation over a transonic compressor blade by conditionally averaged PIV and high-speed shadowgraphs
The impact of separation control has been investigated in a highly loaded transonic compressor cascade at an inlet Mach number of 1.21 and a chord based Reynolds number of 1.4 × 106. Applied control devices are air jet vortex generators (AJVG) and a surface roughness patch. Comparative flows without
Conceptio Open Archive
Analyze & explore related research in Conceptio
Connect this record directly into your research workflow or AI agent. Explore citations across open repositories, query full text, and export structured proof bundles.
This document is indexed with metadata only: full text is not available in the archive for this record. Open the official source ↗
Related documents
- The secondary flow in compressor blades at high negative incidences#491649
- The Design of an Ultra-High-Pressure Jet-Stirred Reactor for the Study of Supercritical Pressure Combustion Kinetics#291215
- Early Gastric Decompression During Advanced Cardiopulmonary Resuscitation (EGD_ACLS)#1173511
- Experimental Data of Supercritical Carbon Dioxide (sCO2) Compressor at Various Fluid States - Supplementary Data#349114
- Compression Feedback for Patients With In-hospital Cardiac Arrest#810715
Record · ID 1089801
Retrieved via Conceptio: every document is proof-bundled with source, license, and retrieval metadata.
Retrieved via Conceptio: every document is proof-bundled with source, license, and retrieval metadata.
Bring this data into your agent: Connect via MCP or API · 20 free credits to start · no card required
Read the Docs → · View CLI source on GitHub · Conceptio Open Knowledge Archive
Read the Docs → · View CLI source on GitHub · Conceptio Open Knowledge Archive