Extended Conical Flow Theory for Design of Pressure Probes in Supersonic Flows with Moderate Flow Angularity and Swirl
47th AIAA Aerospace Sciences Meeting and the New Horizons Forum and Aerospace Exhibit 2009 ; 2009 ; Orlando, FL
47th AIAA Aerospace Sciences Meeting and the New Horizons Forum and Aerospace Exhibit 2009 ; 12564-12573
2009-01-01
10 pages
Includes bibliographical references and index; Also contains papers from the New Horizons Forum and Aerospace Exhibit 2009
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Calibration of hemispherical-head flow angularity probes
AIAA | 1992
|Mach Flow Angularity Probes for Scramjet Engine Flow Path Diagnostics
SAE Technical Papers | 1993
|