Table of Contents Table of Contents
Previous Page  10 / 11 Next Page
Information
Show Menu
Previous Page 10 / 11 Next Page
Page Background

В.Б. Сапожников, Н.И. Авраамов

10

Инженерный журнал: наука и инновации

# 2·2017

Conditions for gas cavity collapse in fluid during

the transition from weightlessness to short-term

exposure to individual G-force pulses

©V.B. Sapozhnikov, N.I. Avraamov

BaumanMoscowState Technical University, 105005, Moscow, Russia

We present experimental investigation results for the gas cavity collapse processes in

propellant tanks of liquid propellant rocket propulsion plants under free (nonperturbed)

orbital (suborbital) flight conditions, subjected to short-term individual g-force pulses.

We defined the structure of dimensionless groups that link the maximum cavity volume to

the amplitude and duration of a g-force pulse and to the physical properties of the fluid,

so that the cavity does not collapse under the influence of the buoyant force when floating

up. We carried out our experimental investigation using a weightlessness bench imple-

menting reduced gravity conditions during free fall of the equipment being tested, and

employing a flying laboratory moving along a Keplerian parabola. Results of the experi-

mental studies mean that the nature of the collapse process in the case of free gas cavities

subjected to individual g-force pulses is determined by the dimensionless pulse duration

value and by the surface tension to viscosity ratio. Short-term g-force pulses make it pos-

sible to disregard the effect of viscosity upon the gas cavity collapse process. The cavity

collapse, if it takes place, happens when the pulse duration is over, and is caused by fluid

motion in the bottom hemisphere of the cavity. When the g-force pulse duration is signifi-

cant, the pulse-induced cavity motion in the fluid becomes quasi-stationary, and the free

surface stability is determined by the mass-force field intensity, the capillary viscosity ra-

dius parameter being fixed.

Keywords:

liquid propellant rocket propulsion plant, propellant tank, weightlessness,

g-force, gas cavity, strain, collapse, experimental studies

REFERENCES

[1]

Korolkov A.V., Sapozhnikov V.B.

Vestnik Moskovskogo gosudarstvennogo uni-

versiteta lesa / Lesnoy vestnik: Moskovskiy gosudarstvennyy universitet lesa

(Mytishchi) — Moscow state forest university bulletin / Lesnoy vestnik

, 2005,

no. 4, pp. 51–52.

[2]

Sapozhnikov V.B., Korolkov A.V. Mathematical modeling of a spacecrafts’ fuel

tank empty in-gin the orbital flight conditions

. International Scientific Confer-

ence “Physical and Mathematical Problems of Advanced Technology Develop-

ment” (Moscow, Bauman MSTU, 17–19 November 2014): abstracts

. Moscow,

BMSTU Publ., 2014, pp. 80–81.

[3]

Sedov L.I.

Metody podobiya i razmernosti v mekhanike

[Similarity and dimensional

methods in mechanics]. 8th ed., revised. Moscow, Nauka Publ., 1977, 440 p.

[4]

Sapozhnikov V.B., Korolkov A.V.

Sovremennaya nauka: issledovaniya, idei,

rezultaty, tekhnologii — Modern Science: Researches, Ideas, Results, Technolo-

gies

, 2014, no. 1 (14), pp. 60–65.

[5]

Ganiev R.F., Lapchinskiy G.F.

Problemy mekhaniki v kosmicheskoy tekhnologii

[Problems of mechanics in space technology]. Moscow, Mashinostroenie Publ.,

1978, 119 p.

[6]

Voinov O.V. Conditions for breakdown of a spherical gas bubble in fluid caused

by nonlinear pulsations.

Doklady Physics

, 2008, vol. 53, no. 10, pp. 539–543.

DOI: 10.1134/S1028335808100108 [In Russ.: Voinov O.V. Usloviya razrusheni-