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Comparison of wind-tunnel test results at M[subscript infinity] = 0.7 with results from the Boeing TEA-230 subsonic flow method

Title:Comparison of wind-tunnel test results at M[subscript infinity] = 0.7 with results from the Boeing TEA-230 subsonic flow method
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Note:National Aeronautics and Space Administration ;, 1975
  
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Subject:Aerodynamic load
Subject:Aerodynamics
Subject:Airplanes -- Nacelles
Subject:Jet transports -- Design and construction
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