A Review on the Change Process and the Evolution of Aircraft Engine Air Intake
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Moradi M. Booklet: The Developmental Process of Fighter Design. Tehran: Imam Hossein University.
http://www.aerospacetalk.ir/vb/showthread.php?t=36647
Seddon J, Goldsmith EL. Intake Aerodynamics. London: Collins Professional and Technical Books; 1985.
Chambers JR. Partners in Freedom—Contributions of the Langley Research Center to, U.S. Military Aircraft of the 1990s, Monographs in Aerospace History, SP-2000-4519. NASA; 2000.
Geddes JP. Boeing Sells a Thousand 727s—and Hopes to Sell Plenty More. Interavia, Aerosp World Business Technol. 1976; 28(3): 245–247p.
Sacks AH, Spreiter JR. Theoretical Investigation of Submerged Inlets at Low Speeds, NACA Technical Note 2323. NASA; 1951.
Ward-Smith AJ. A prediction method for the influence of a turbulent boundary layer on the efficiency of submerged intakes. Aeronaut J. 1973; 77: 570–574p.
Stewart RL. A Flight Comparison of a Scoop Inlet and a Submerged Inlet at Transonic Speeds, NACA Research Memorandum A53A06. NASA; 1953.
Bore CL. Intakes for vertical landing aircraft. In: E.L. Goldsmith, J. Seddon, editors. Practical Intake Aerodynamic Design. Oxford: Blackwell Scientific Publications; 1993.
Curtis P, Whitmore I. The Development of the Nimrod MRA.4 Intake. In: 7th CEAS European Propulsion Forum, Council of European Aerospace Studies, Pau, France. 1999, pp. 1–10.
Whitford R. Design for Air Combat. London: Jane’s; 1987.
Ran H, Mavris D. Preliminary Design of a 2D Supersonic Inlet to Maximize Total Pressure Recovery, AIAA Paper 2005-7357. 2005.
Hawkins JE. YF-16 inlet design and performance. J Aircraft. 1976; 13(6): 436–441p.
Mattingly JD. Elements of Gas Turbine Propulsion. New York: McGraw–Hill; 1996.
Jenkins RC, Loeffler AL. Modeling of subsonic flow through a compact offset inlet diffuser. AIAA J. 1991; 29(3): 401–408p.
Zhang WL, Knight D, Smith D. Automated design of a three-dimensional subsonic diffuser. J Propul Power. 2000; 16(6): 1132–1140p.
Lefantzi S, Knight DD. Automated design optimization of a three-dimensional s-shaped subsonic diffuser. J Propul Power. 2002; 18(4): 913p.
Zha G-C, Smith D, Schwabacher M, Rasheed K, Gelsey A, Knight D, Haas M. High-performance supersonic missile inlet design using automated optimization. J Aircraft. 1997; 34(6): 697–705p.
Haines AB. Aerodynamics. Aeronaut J. 1976; 80: 277–293p.
Eleshaky ME, Baysal O. Shape optimizing nacelle near flat- plate wing using multiblock sensitivity analysis. J Aircraft. 1998; 35(1): 33–38p.
Imfield WF. Development program for the F-15 inlet. J Aircraft. 1976; 13(4): 286p.
Scherz CJ, Williams LE. Digital Computer Application in the F-15 engine air inlet control system. J Guidance Control. 1978; 1(6): 420p.
Segal C. Aircraft engine bay cooling and ventilation: design and modeling. J Aircraft. 1997; 34(1): 141–144p.
Hamstra JW, Sylvester TG. System and method for diverting boundary layer air, U.S. Patent No. 5, 779, 189, granted 14 July 1998.
DOI: https://doi.org/10.37628/ijmd.v4i1.628
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