You might also like

More about Cavity Coupled Aeroramp Injector Combustion Study

• Book details
• Synopsis
• Trending among others

You get 172 loyalty points

Book synopsis

The difficulties with fueling of supersonic combustion ramjet engines with hydrocarbon based fuels presents many challenges that are currently being tackled by the Air Force Research Lab Propulsion Directorate Aerospace Propulsion Division. As the scramjet engine designs are scaled up, the need for a better solution to supersonic mixing has led to the development of many different styles of fuel injection. An aerodynamic ramp injector has been shown to have a quantitative improvement over a physical ramp while still achieving desirable mixing characteristics. The objectives for this research was quantifying the performance and operability implications of replacing four 15 degree round injectors with four arrays of improved aeroramp injectors. Ignition limits and pre-combustion shock position were used to define the operability differences while combustion efficiency was the primary metric used for performance comparisons.

Book details

Book category Knihy po anglicky Society & social sciences Education

• Full title: Cavity Coupled Aeroramp Injector Combustion Study
• Author: Dell T Olmstead
• Language: English
• Binding: Paperback
• Number of pages: 80
• EAN: 9781288286218
• ISBN: 9781288286218
• ID: 08241212
• Publisher: Biblioscholar
• Weight: 159 g
• Dimensions: 246 × 189 × 4 mm
• Date of publishing: 01. November 2012

Trending among others

---

---

---