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Flight tests of a twin-duct induction system for a mach number range of 0.78 to 2.07

Title:Flight tests of a twin-duct induction system for a mach number range of 0.78 to 2.07
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Note:National Aeronautics and Space Administration, 1960
  
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Subject:Fighter planes -- Flight testing
Subject:Jet engines -- Air intakes -- Testing
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