N. I. Tillyaeva: search on Z-Library

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1

Contouring the nozzles producing a uniform supersonic flow or a thrust maximum in the presence of a curvilinear sonic line

A. A. Kraiko, A. N. Kraiko, K. S. P’yankov, N. I. Tillyaeva

Journal:

Year:

2012

Language:

english

File:

PDF, 328 KB

english, 2012

2

Shape of supersonic parts of axisymmetric nozzles for nonuniform and swirling flows

N. I. Tillyaeva

Journal:

Year:

1975

Language:

english

File:

PDF, 646 KB

english, 1975

3

Comparison of integrated characteristics and shapes of profiled contours of laval nozzles with “smooth” and “abrupt” contractions

A. N. Kraiko, N. I. Tillyaeva, S. A. Shcherbakov

Journal:

Year:

1986

Language:

english

File:

PDF, 944 KB

english, 1986

4

Allowance for nonuniformity of the flow at the minimal section in optimal profiling of the expanding part of a nozzle

A. N. Kraiko, N. N. Tillyaeva

Journal:

Year:

1982

Language:

english

File:

PDF, 400 KB

english, 1982

5

On profiling supersonic nozzles to achieve uniform flow in the annular exit section

N. I. Tillyaeva, E. Ya. Shironosova

Journal:

Year:

1995

Language:

english

File:

PDF, 172 KB

english, 1995

6

Shock wave structures ahead of nonuniform fan cascades

N. L. Efremov, A. N. Kraiko, K. S. Pyankov, N. I. Tillyaeva, E. A. Yakovlev

Journal:

Year:

2010

Language:

english

File:

PDF, 521 KB

english, 2010

7

On the numerical construction of shock-wave fronts

A.N. Kraiko, V.E. Makarov, N.N. Tillyaeva

Journal:

USSR Computational Mathematics and Mathematical Physics

Year:

1980

Language:

english

File:

PDF, 620 KB

english, 1980

8

Variational problem of optimum side wall design for a narrow three-dimensional nozzle

A. N. Kraiko, A. R. Polyanskii, N. I. Tillyaeva

Journal:

Year:

1992

Language:

english

File:

PDF, 755 KB

english, 1992

9

Optimal Axisymmetric Noses of Bodies in a Flow. Calculations and Experiments

Bol’shiyanov, I. P., Zakharov, N. N., P’yankov, K. S., Tillyaeva, N. I.

Journal:

Year:

2018

Language:

english

File:

PDF, 1.05 MB

english, 2018

10

Conjugate Problem for Lagrange Multipliers and Consequences for Partial Differential Equations of Mixed Type

Kraiko, A. N., Tillyaeva, N. I.

Journal:

Journal of Mathematical Sciences

Year:

2015

Language:

english

File:

PDF, 832 KB

english, 2015

11

A method of computing ideal gas flows in plane and axisymmetric nozzles with contour breaks

A.N. Kraiko, N.I. Tillyaeva, S.A. Shcherbakov

Journal:

USSR Computational Mathematics and Mathematical Physics

Year:

1986

Language:

english

File:

PDF, 1.19 MB

english, 1986

12

Minimum-drag cascade design for supersonic flow with subsonic normal velocity component

A. N. Kraiko, D. E. Pudovikov, N. I. Tillyaeva

Journal:

Year:

1995

Language:

english

File:

PDF, 631 KB

english, 1995

13

Axisymmetric-conical and locally conical flows without swirling

Kraiko, A. N., Tillyaeva, N. I.

Journal:

Journal of Applied Mechanics and Technical Physics

Year:

2014

Language:

english

File:

PDF, 541 KB

english, 2014

14

Calculation of supersonic gas flow over a ducted body in regimes with a detached shock wave

N. I. Tillyaeva

Journal:

Year:

1981

Language:

english

File:

PDF, 467 KB

english, 1981

15

Stability of supersonic ideal-gas flow past cylindrical channels and cavities with a bow shock

V. T. Grin', N. N. Slavyanov, N. I. Tillyaeva

Journal:

Year:

1987

Language:

english

File:

PDF, 600 KB

english, 1987

16

Comparison of the efficiencies of spike and combined annular nozzles

Tillyaeva, N. I.

Journal:

Year:

2017

Language:

english

File:

PDF, 452 KB

english, 2017

17

Solution of the problem of interaction between a supersonic jet and an obstacle of finite dimensions

L. I. Derbeneva, M. Yu. Kurshakov, N. I. Tillyaeva, Yu. N. Shishkin

Journal:

Year:

1986

Language:

english

File:

PDF, 564 KB

english, 1986

18

Contouring two-sided asymmetric plane maximum-thrust nozzles

Kraiko, A. A., Pyankov, K. S., Tillyaeva, N. I.

Journal:

Year:

2016

Language:

english

File:

PDF, 482 KB

english, 2016

19

Designing three-dimensional nozzles to achieve near-uniform supersonic or hypersonic flow in the rectangular exit section

M. K. Aukin, A. N. Kraiko, D. A. Lubimov, V. E. Makarov, N. I. Tillyaeva

Journal:

Year:

1995

Language:

english

File:

PDF, 645 KB

english, 1995

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