Use of temperature-sensitive coatings for obtaining quantitative aerodynamic heat- transfer data
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Va.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.2558
Reference8 articles.
1. A Simple Method of Estimating the Vortex Intensity
2. Todd, K. W. "Some developments in instrumentation in air flow analysis/' Proc. Inst. Mech. Engrs. (London) 161, 213(1949).
3. Lakshminarayana, B. "Leakage and secondary flows in axial compressor cascades/' Ph.D. Thesis, Liverpool Univ. (September 1963).
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