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pro vyhledávání: '"D. L. Hovland"'
Publikováno v:
Journal of Propulsion and Power. 8:954-960
Particle size distributions were measured in the combustion chamber, exhaust nozzle, and exhaust plume of a small, two-dimensional rocket motor that utilized aluminized propellants. Various nozzle contours and pressures to 4.36 MPa were utilized. For