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Continuous-output terminal-shock-position sensor for mixed-compression inlets evaluated in wind-tunnel tests of YF-12 aircraft inlet

Title:Continuous-output terminal-shock-position sensor for mixed-compression inlets evaluated in wind-tunnel tests of YF-12 aircraft inlet
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Note:National Aeronautics and Space Administration ;, 1974
  
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Subject:Aerodynamics, Supersonic
Subject:Detectors
Subject:Jet engines -- Air intakes
Subject:SR-71 Blackbird (Jet reconnaissance plane)
Subject:Shock waves -- Measurement -- Equipment and supplies
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