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An investigation of the effectiveness of several devices in simulating a rocket plume at free stream Mach numbers 0.9 to 1.2

Title:An investigation of the effectiveness of several devices in simulating a rocket plume at free stream Mach numbers 0.9 to 1.2
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Note:Redstone Arsenal, Alabama ; U.S. Army Missile Command, 1971., 1971
  
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Subject:Aerodynamics, Transonic
Subject:Rocket engines -- Exhaust emissions
Subject:Rockets (Aeronautics) -- Nozzles
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