TURBULENT BOUNDARY LAYER COMBUSTION IN THE HYBRID ROCKET
- 1 January 1963
- book chapter
- Published by Elsevier
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- The Turbulent Boundary Layer on Chemically Active Ablating SurfacesJournal of the Aerospace Sciences, 1961
- The Effect of Mass Transfer on the Compressible Turbulent Boundary-Layer Skin Friction and Heat TransferJournal of the Aeronautical Sciences, 1954
- An Approximate Theory of Porous, Sweat, or Film Cooling With Reactive FluidsJournal of the American Rocket Society, 1952
- 7. Bericht über Untersuchungen zur ausgebildeten TurbulenzZAMM - Journal of Applied Mathematics and Mechanics / Zeitschrift für Angewandte Mathematik und Mechanik, 1925