محرك (ترتيب اسطوانات خطي) (Arabic Wikipedia)

Analysis of information sources in references of the Wikipedia article "محرك (ترتيب اسطوانات خطي)" in Arabic language version.

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com.jm

books.google.com.jm

  • Wilkinson، Stephan (2005). "DB-601". Man And Machine: The Best of Stephan Wilkinson. Globe Pequot. ص. 174. ISBN:1-59228-812-X. مؤرشف من الأصل في 2020-04-26. اطلع عليه بتاريخ 2013-01-24. The widest part of the engine–the two banks of cylinder heads–were down near the already wide midline of the fuselage.
  • Meyers، W. G. (سبتمبر 1925). Mitchell، Harley W. (المحرر). "Future Possibilities in Aircraft Engine Design". Aeronautics. Chicago, IL USA: Aeronautical Publications. ج. 5 ع. 3: 85. مؤرشف من الأصل في 2020-04-26. اطلع عليه بتاريخ 2013-01-24. (4) Its high center of thrust insures better flying qualities by offsetting a tendency of the ship to climb when full power is suddenly thrown on,

racingcampbells.com

  • "Napier Lion". The Racing Campbells. مؤرشف من الأصل في 2009-09-14. اطلع عليه بتاريخ 2012-06-30. The Lion was a 12-cylinder W-block inline aircraft engine built by Napier & Son starting in 1917, and ending in the 1930s. {{استشهاد ويب}}: روابط خارجية في |عمل= (مساعدة)

web.archive.org

  • "Napier Lion". The Racing Campbells. مؤرشف من الأصل في 2009-09-14. اطلع عليه بتاريخ 2012-06-30. The Lion was a 12-cylinder W-block inline aircraft engine built by Napier & Son starting in 1917, and ending in the 1930s. {{استشهاد ويب}}: روابط خارجية في |عمل= (مساعدة)
  • Wilkinson، Stephan (2005). "DB-601". Man And Machine: The Best of Stephan Wilkinson. Globe Pequot. ص. 174. ISBN:1-59228-812-X. مؤرشف من الأصل في 2020-04-26. اطلع عليه بتاريخ 2013-01-24. The widest part of the engine–the two banks of cylinder heads–were down near the already wide midline of the fuselage.
  • Meyers، W. G. (سبتمبر 1925). Mitchell، Harley W. (المحرر). "Future Possibilities in Aircraft Engine Design". Aeronautics. Chicago, IL USA: Aeronautical Publications. ج. 5 ع. 3: 85. مؤرشف من الأصل في 2020-04-26. اطلع عليه بتاريخ 2013-01-24. (4) Its high center of thrust insures better flying qualities by offsetting a tendency of the ship to climb when full power is suddenly thrown on,