ScholarLens Back to search
1951•Unpublished venueRequires access

Altitude-test-chamber Investigation of Performance of a 28-inch Ram-jet Engine IV : Effect of Inlet-air Temperature, Combustion-chamber-inlet Mach Number, and Fuel Volatility on Combustion Performance

Robert W Kahn, S. Nakanishi, James L. Harp

Open publisher page 0 citations

Abstract

Report presenting testing of the effects of the following variables on combustion performance are determined: inlet-air temperature, combustion-chamber-inlet Mach number and pressure, and fuel density and volatility.

About this research paper

What this paper is about

Report presenting testing of the effects of the following variables on combustion performance are determined: inlet-air temperature, combustion-chamber-inlet Mach number and pressure, and fuel density and volatility.

Why it matters

A significance statement is not available in the OpenAlex record.

Key contribution

A contribution statement is not available in the OpenAlex record.

Method / approach

Method details are not available in the OpenAlex metadata.

Main findings

Findings are not separately available in the OpenAlex metadata.

Limitations

Limitations are not available in the OpenAlex metadata.

Applications

Application details are not available in the OpenAlex metadata.

Available abstract

Report presenting testing of the effects of the following variables on combustion performance are determined: inlet-air temperature, combustion-chamber-inlet Mach number and pressure, and fuel density and volatility.

Key concepts: Inlet, Combustion chamber, Mach number, Jet engine, Combustion, Mechanics, Environmental science, Nuclear engineering

Related papers

Related paper 1Related paper 2Related paper 3
Back to paper searchBrowse research topicsOriginal source
Altitude-test-chamber Investigation of Performance of a 28-inch Ram-jet Engine IV : Effect of Inlet-air Temperature, Combustion-chamber-inlet Mach Number, and Fuel Volatility on Combustion Performance — Research Paper | ScholarLens