BASE FLOW CHARACTERISTICS FOR SEVERAL FOURCLUSTERED ROCKET CONFIGURATIONS AT MACH NUMBERS FROM 2.0 TO 3.5
Abstract
A generalized study of base flow phenomena was conducted with four 500-pound-thrust JP-4 fuel - liquid-oxygen rocket motors installed in the base of a 12-inch-diameter cylindrical model. Data were obtained over a Mach number and nozzle pressure ratio range of 2.0 to 3.5 and 340 to 6800, respectively. Base heat flux, gas temperature, and pressure were highest in the center of the cluster core and decreased in a radial direction. Although a maximum heat flux of 93 Btu per square foot per second was measured within the cluster core, peripheral heat fluxes were low, averaging about 5 Btu per square foot per second for all configurations. Generally base heat flux was found to be independent of Mach number over the range investigated. Base heat flux within the cluster core was decreased by increasing motor spacing, motor extension, a combination of increasing nozzle area ratio and decreasing exit angle, and gimbaling the two side engines. Small amounts of nitrogen injected within the cluster core sharply reduced core heat flux. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Dec 01, 1961
- Accession Number
- AD0267304
Entities
People
- James J. Ward
- Norman T. Musial
Organizations
- National Aeronautics and Space Administration