A Method for Analyzing the Heat Insulating Properties of the Laminar Compressible Boundary Layer
- 1 December 1954
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 21 (12), 825-834
- https://doi.org/10.2514/8.3229
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- A Table of the Complete Cicala FunctionJournal of the Aeronautical Sciences, 1953
- The Subsonic Calculation of Circulatory Spanwise Loadings for Oscillating Airfoils by Lifting-Line TechniquesJournal of the Aeronautical Sciences, 1952
- On Heat Transfer over a Sweat-Cooled Surface in Laminar Compressible Flow with a Pressure GradientJournal of the Aeronautical Sciences, 1952
- Heat Transfer to Constant-Property Laminar Boundary-Layer Flows with Power-Function Free-Stream Velocity and Wall-Temperature VariationJournal of the Aeronautical Sciences, 1952