Tests of a Small-scale NACA Submerged Inlet at Transonic Mach Numbers PDF Download
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Author: L. Stewart Rolls
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 22
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Book Description
The pressure-recovery characteristics at the vertical center line of an NACA submerged inlet of aspect ratio 5 have been measured in the Mach number range 0.60 to 1.08 by the wing-flow method. The variation of ram-recovery ratio determined from measurements at the center line of the inlet with test station Mach number is presented for mass-flow ratios of 0.30 to 0.60.
Author: L. Stewart Rolls
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 22
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Book Description
The pressure-recovery characteristics at the vertical center line of an NACA submerged inlet of aspect ratio 5 have been measured in the Mach number range 0.60 to 1.08 by the wing-flow method. The variation of ram-recovery ratio determined from measurements at the center line of the inlet with test station Mach number is presented for mass-flow ratios of 0.30 to 0.60.
Author:
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ISBN:
Category : Aerodynamics
Languages : en
Pages : 36
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Author: United States. National Advisory Committee for Aeronautics
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ISBN:
Category : Aeronautics
Languages : en
Pages : 580
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Author: Donald E. Gault
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Category : Aeronautics
Languages : en
Pages : 40
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Author: Warren E. Anderson
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Category :
Languages : en
Pages : 29
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Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 818
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Author: United States. National Advisory Committee for Aeronautics
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ISBN:
Category : Aeronautics
Languages : en
Pages : 568
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Author: United States. National Advisory Committee for Aeronautics
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ISBN:
Category : Aeronautics
Languages : en
Pages : 508
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Author: Richard J. Re
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Category : Aerofoils
Languages : en
Pages : 116
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Category :
Languages : en
Pages : 524
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