Correlation of Base Pressure and Wake Structure of Sharp- and Blunt-Nose Cones with Reynolds Number Based on Boundary-Layer Momentum Thickness
- 1 March 1959
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 26 (3) , 185-186
- https://doi.org/10.2514/8.7990
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- A PROCEDURE FOR CALCULATING THE BOUNDARY-LAYER DEVELOPMENT IN THE REGION OF TRANSITION FROM LAMINAR TO TURBULENT FLOWPublished by Defense Technical Information Center (DTIC) ,1957
- A THEORETICAL INVESTIGATION OF TURBULENT BOUNDARY LAYER FLOW WITH HEAT TRANSFER AT SUPERSONIC AND HYPERSONIC SPEEDSPublished by Defense Technical Information Center (DTIC) ,1955
- A Mixing Theory for the Interaction Between Dissipative Flows and Nearly Isentropic StreamsJournal of the Aeronautical Sciences, 1952
- Interrelationship Between Boundary Layer and Base PressureJournal of the Aeronautical Sciences, 1951