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  • Other Sources  (2)
  • 2010-2014
  • 1940-1944  (2)
  • 1942  (2)
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  • 2010-2014
  • 1940-1944  (2)
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  • 1
    Publication Date: 2019-06-28
    Description: The drag characteristics of eight radial-engine cowlings have been determined over a wide speed range in the NACA 8-foot high-speed wind tunnel. The pressure distribution over all cowlings was measured, to and above the speed of the compressibility burble, as an aid in interpreting the force tests. One-fifth-scale models of radial-engine cowlings on a wing-nacelle combination were used in the tests.
    Type: NACA-TR-745
    Format: application/pdf
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  • 2
    Publication Date: 2019-06-28
    Description: Report presents the results of tests made to determine the drag of closed-cockpit and transport-type windshields. The tests were made at speeds corresponding to a Mach number range of approximately 0.25 to 0.58 in the NACA 8-foot high-speed wind tunnel. This speed range corresponds to a test Reynolds number range of 2,510,000 to 4,830,000 based on the mean aerodynamic chord of the full-span model (17.29 in.). The shapes of the windshield proper, the hood, and the tail fairing were systematically varied to include common types and refined design.
    Type: NACA-TR-730
    Format: application/pdf
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