Method of reducing design aerodynamic characteristics to the results of drain tests of a transport category aircraft model

Abstract


A method of reducing design aerodynamic characteristics to the results of drain tests by adjusting a mathematical model of the aircraft being designed on the basis of an aerodynamic prototype is presented in the paper.


About the authors

Yu. I. Bondar

National Technical University of Ukraine “Kiev Polytechnic Institute”

Author for correspondence.
Email: bomis@meta.ua

Ukraine

Senior Lecturer

Department of Aerospace System

References

  1. Bondar Y.I, Evdokimov S.A., Prikhodko S.L. Calculation of intensity of the vortical system of AN-2 plane for the optimisation of locating the outboard equipment when carrying out agricultural chemical treatment // Coll. scientif. works. «Aircraft Application in a national economy», MAP, GOSNIIGA, Art.268. M., 1987. P.60-72 (In Russ.)
  2. Isaev S.I., Mironov B.М, Nikitin V.M. Osnovy termodinamiki, gazovoy dinamiki i teploperedachi. [Foundations of thermodynamics, gas dynamics and thermal transfer]. M.: Mashinostroenie Publ. 1968. 275 p.
  3. Lock R.C., Firmin M.C.P. Survey of techniques for estimating viscous effects in external aerodynamics. Proceedings of IMA Conference on Numerical Methods in Aeronautical Fluid Dynamics, 30 March - 1 April 1981, edited by P. Roe, Academic Press, 1983.
  4. Lyapunov S.V., Mikhaylov Y.S. Calculation of a transonic continuous flow around a profile taking viscosity into account // Тrudy CAGI. 1984. Is. 2254. 48 p. (In Russ.)
  5. Lighthill M.J. On displacement thickness // J. Fluid Mech. 1958. V.4. Р. 383. doi: 10.1017/S0022112058000525
  6. Green J.E., Weeks D.J., Brooman J.W.F. Prediction of turbulent boundary layers and wakes in compressible flow by a lagentrainment method // RAE Technical Report 72231 (ARC-RM 3791), 1977.
  7. Williams B.R. The prediction of separated flow using a viscous-inviscid interaction method. ICAS-84-2.3.3, 1984.
  8. Cross A.G.T. Boundary layer calculation and viscous-inviscid coupling. ICAS-86-2.4.1, 1986.
  9. Drela M., Giles M.B. Viscous-inviscid analysis of transonic and low Reynolds number airfoils // AIAA Journal. 1987. V. 25, No. 10. Р. 1347-1355. doi: 10.2514/3.9789
  10. Galkin V.M, Krymasova G.V. Implementation of a program of calculation of a laminar and turbulent boundary layer, passage and track on micro-computer APPLE-II and possibility of development of its computational capability. NTO-1250 dcp., 1985.(In Russ.)
  11. Lyapunov S.V. Calculation of wave a resistance in case of transonic flow around the profile with the application of nonconservative difference circuits // NТО CAGI N-7561, 1987. (In Russ.)
  12. Cooke J.C. The drag of infinite swept wings, with a addendum. ARC.CP N-1040, 1964.
  13. Bokser V.D, Serebpiyskiy J.M. An approximate method of determining wave drag with a local supersonic zone // Scientific notes of TsAGI. V. IX, no. 5, 1978. (In Russ.)

Statistics

Views

Abstract - 56

PDF (Russian) - 27

Article Metrics

Metrics Loading ...

PlumX

Dimensions

Refbacks

  • There are currently no refbacks.

Copyright (c) 2015 VESTNIK of the Samara State Aerospace University

This website uses cookies

You consent to our cookies if you continue to use our website.

About Cookies