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Langley 9-inch supersonic tunnel tests of several modifications of a supersonic missile having tandem cruciform lifting surfaces : three-component data results of models having ratios of wing span to tail span less than 1

Title:Langley 9-inch supersonic tunnel tests of several modifications of a supersonic missile having tandem cruciform lifting surfaces : three-component data results of models having ratios of wing span to tail span less than 1
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Note:National Advisory Committee for Aeronautics, 1960
  
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Subject:Airplanes -- Wings, Cruciform
Subject:Rockets (Aeronautics) -- Testing
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