SU605144A1 - Method of dynamic testing of structure with cylindrical internal channel - Google Patents

Method of dynamic testing of structure with cylindrical internal channel

Info

Publication number
SU605144A1
SU605144A1 SU762356073A SU2356073A SU605144A1 SU 605144 A1 SU605144 A1 SU 605144A1 SU 762356073 A SU762356073 A SU 762356073A SU 2356073 A SU2356073 A SU 2356073A SU 605144 A1 SU605144 A1 SU 605144A1
Authority
SU
USSR - Soviet Union
Prior art keywords
internal channel
cylindrical internal
dynamic testing
moving
testing
Prior art date
Application number
SU762356073A
Other languages
Russian (ru)
Inventor
Анатолий Трофимович Перчун
Original Assignee
Серпуховское Высшее Военное Командное Училище Имени Ленинского Комсомола
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Серпуховское Высшее Военное Командное Училище Имени Ленинского Комсомола filed Critical Серпуховское Высшее Военное Командное Училище Имени Ленинского Комсомола
Priority to SU762356073A priority Critical patent/SU605144A1/en
Application granted granted Critical
Publication of SU605144A1 publication Critical patent/SU605144A1/en

Links

Landscapes

  • Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)
  • Investigating Or Analyzing Materials By The Use Of Ultrasonic Waves (AREA)

Description

приводит к образованию перемещающегос  фронта ударной волны, на котором скачкообразно измен етс  давление. Воздействие на исследуемую конструкцию 1 перемещающегос  фронта ударной волны соответствует воздействию сверхзвуковой осесимметричной равномерно распределенной но длине внутреннего канала 5 конструкцин 1 подвижной нагрузки.leads to the formation of a moving front of the shock wave, on which the pressure changes abruptly. The impact on the test structure 1 of a moving shock wave front corresponds to the action of a supersonic axisymmetric evenly distributed but the length of the internal channel 5 of the design of the moving load.

Величина скачка давлени  на фронте ударной волны зависит от соотношени  давлений и примен емых газов в камерах 2 и 3 низкого и высокого давлений. Возникающие в материале конструкции 1 деформации фиксируютс  датчиками 6, 7 и 8 и в виде электрического сигнала поступают в измерительную аппаратуру 9.The magnitude of the pressure jump at the shock wave front depends on the ratio of pressures and used gases in chambers 2 and 3 of low and high pressures. The deformations arising in the material of construction 1 are recorded by sensors 6, 7 and 8 and are transferred to measuring equipment 9 as an electrical signal.

Применение ударной трубы дл  воздействи  на конструкцию по предлагаемому способу позвол ет создавать на их внутреннем канале сверхзвуковые осесимметричные подвижные нагрузки.The use of a shock tube to influence the structure of the proposed method allows one to create supersonic axisymmetric moving loads on their internal channel.

4four

Claims (2)

1.Авторское свидетельство СССР № 88551, кл. G 01N 3/12, 1950.1. USSR author's certificate number 88551, cl. G 01N 3/12, 1950. 2.Патент США № 3400574, кл. 73-40.5, 1968.2. US patent number 3400574, cl. 73-40.5, 1968.
SU762356073A 1976-05-03 1976-05-03 Method of dynamic testing of structure with cylindrical internal channel SU605144A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU762356073A SU605144A1 (en) 1976-05-03 1976-05-03 Method of dynamic testing of structure with cylindrical internal channel

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU762356073A SU605144A1 (en) 1976-05-03 1976-05-03 Method of dynamic testing of structure with cylindrical internal channel

Publications (1)

Publication Number Publication Date
SU605144A1 true SU605144A1 (en) 1978-04-30

Family

ID=20659891

Family Applications (1)

Application Number Title Priority Date Filing Date
SU762356073A SU605144A1 (en) 1976-05-03 1976-05-03 Method of dynamic testing of structure with cylindrical internal channel

Country Status (1)

Country Link
SU (1) SU605144A1 (en)

Similar Documents

Publication Publication Date Title
Kenner et al. Impact on a simple physical model of the head
ATE18801T1 (en) ARRANGEMENT FOR MEASUREMENT OF THE PRESSURE PROCESS IN CYLINDER-SHAPED HOLLOW BODIES.
SU605144A1 (en) Method of dynamic testing of structure with cylindrical internal channel
NO943613D0 (en) Apparatus for measuring thermodynamic properties in a hydrocarbon sample
JPS5230488A (en) Circumferential length type radial strain measuring apparatus
JPS5324884A (en) Hardness tester
JPS5436782A (en) Torsion tester
Surkin et al. Experimental investigation of dynamical stability of spherical segments
SU794483A2 (en) Acoustic testing stand
RU1768703C (en) Device for measuring stress in earth
SU544881A2 (en) The method of checking the integrity of the circuits of piezoelectric sensors with several sensitivity axes
JPS5524629A (en) Test piece jig for stress corrosion cracking tester of constant speed type
SU1280518A2 (en) Device for determining elastic characteristics of materials
ZIMMERMANN Gas pressure measurement(of pressure bomb in conjunction with copper cylinder deformation test)
ALEKSANDROV et al. Investigation of strains and stresses by the method of photoelastic coatings/Survey
Breitbach et al. Modal survey tests on the spacecraft structure ITOS RCA 1769 701
SU521184A1 (en) Method for measuring body weight under weightless conditions
SU582477A1 (en) Method of measuring hardness
RICKS Teledyne Taber 206-1000 and 2210-3000 pressure transducer proof test and burst test(Final Test Report)
RU2040782C1 (en) Pressure transducer
JPS5340901A (en) Chassis dynamometer
Farid An investigation into the effect of enclosed lamination in Larssen sheet pile
ZIAAI-MOAYYED Back stresses in monotonic and cyclic deformation: Transient and steady state behavior[Ph. D. Thesis]
HOFFMAN Self-supporting strain transducer[Patent]
HEINRICH et al. Functioning of the omega sensor on textile samples under high loading rates[Final Report, Jul. 1973- May 1974]