Aerodynamic interference between a system of bodies of revolution in an unsteady subsonic flow

Butoescu, Valentin Adrian Jean; Popescu, Florica

doi:10.1016/s0362-546x(97)00218-6

Cited by 2 publications

(3 citation statements)

References 2 publications

Supporting

Mentioning

Contrasting

Order By: Relevance

“…This last case is presented in [14] and it will be analyzed in a further paper when we will discuss the unsteady aerodynamic interference problem. The present article resumes and enhances some original ideas the author firstly treated in [6]- [9]. In the meanwhile, he has made some improvements regarding the numerical approach and mathematical presentation.…”

Section: Incas Bulletin Volume 9 Issue 1/ 2017mentioning

confidence: 71%

Aerodynamic Interference between Oscillating Lifting Surfaces and Fuselage. Part 6: A Panel Method for Non-Lifting Bodies Oscillating in Subsonic Flow

Butoescu¹

2017

INCAS BULLETIN

View full text Add to dashboard Cite

In the sixth part of this series, we continue our study started in the previous article, i.e., we present the basis of the method for calculating the unsteady airforces on oscillating non-lifting bodies. The method proposed here is a panel one. As it is proved in the previous paper, the potential and velocity induced by a constant source planar panel is composed of two kinds of terms: some of themthe steady terms, can be expressed by the elementary functions; other terms-the unsteady termscannot and should be calculated numerically. The present paper illustrates how the method proposed here can be used in conjunction with the preceding results.

show abstract

Section: Incas Bulletin Volume 9 Issue 1/ 2017mentioning

confidence: 71%

Aerodynamic Interference between Oscillating Lifting Surfaces and Fuselage. Part 6: A Panel Method for Non-Lifting Bodies Oscillating in Subsonic Flow

Butoescu¹

2017

INCAS BULLETIN

View full text Add to dashboard Cite

show abstract

“…Therefore we will seek approximate expressions for the integrals in (8), when the planar domain is bordered by a convex quadrilateral.…”

Section: Incas Bulletin Volume 7 Issue 3/ 2015mentioning

confidence: 99%

“…For lack of time, we have never extended the analysis, except for the case of the body-body interference, [8].…”

Section: Introductionmentioning

confidence: 99%

Aerodynamic Interference between Oscillating Lifting Surfaces and Fuselage Part 5: A Panel Method for Non-Lifting Bodies

Jean¹

2015

INCAS BULLETIN

View full text Add to dashboard Cite

show abstract

Aerodynamic interference between a system of bodies of revolution in an unsteady subsonic flow

Cited by 2 publications

References 2 publications

Aerodynamic Interference between Oscillating Lifting Surfaces and Fuselage. Part 6: A Panel Method for Non-Lifting Bodies Oscillating in Subsonic Flow

Aerodynamic Interference between Oscillating Lifting Surfaces and Fuselage. Part 6: A Panel Method for Non-Lifting Bodies Oscillating in Subsonic Flow

Aerodynamic Interference between Oscillating Lifting Surfaces and Fuselage Part 5: A Panel Method for Non-Lifting Bodies

Contact Info

Product

Resources

About