Main Article Content

Abstract

Statistical data are presented on the number and frontal areas for principal types of manufacturing and constructive imperfections characterizing the condition of aircraft external surface and the level of parasitic drag. Basic laws of varying drag coefficients for various types of surface excrescences as functions of Mach and Reynolds numbers are analyzed. The methodology is considered for evaluating requirements for aircraft surface finish based on the specified level of parasitic drag.

Keywords

No Keywords

Article Details

How to Cite
Fedorenko, G. A. (2023). Parasitic Drag and Requirements for Aircraft External Surface Finish. Journal of Aerospace Sciences and Technologies, 61(1), 232–239. https://doi.org/10.61653/joast.v61i1.2009.637

References

  1. Fedorenko, G. A and Bashkirov, I. G., "Parasitic Drag Prediction", Fundamentals and Computer Code, TsAGI, Russia.
  2. Fedorenko, G. A., "Resistance of Manufacture Imperfections in a Turbulent Boundary Layer", Works of TsAGI, Release 2100, 1981.
  3. Fedorenko, G.A and Pavlenko. I.V., "The Protuberances of an External Surface Aircrafts" (Coefficients of Aerodynamic Drag), Album, TsAGI, 1989.
  4. Fedorenko. G.A., "Parasitic Drag Prediction", Proceeding of Aerospace Technologies Development and Strategies, International Seminar, 05 - 08 February 2003. Bangalore, India.
  5. Fedorenko. G. A., "The Sizes of Technological Zones with Increased Requirements to Quality of Furnish of an External Surface of Wings with Usual and Supercritical Profiles", Technique of Air Fleet, 1991, 3.
  6. Barinov, V. A and Fedorenko. G. A., "Approximate Estimation of the Effect of the Wing and Tail Geometry Deviations from Design Parameters on the Drag Coefficient of Subsonic Airplanes", ISSN 0321 - 3439, Scientists of Note TsAGI, Volume XXII, 2, 1991.

Similar Articles

<< < 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 > >> 

You may also start an advanced similarity search for this article.