Presenter Information

C. Dumas, ONERA

Location

Brunswick, ME

Start Date

1-1-1997 12:00 AM

Description

Increasing rocket engine performance is closely linked to as best a knowledge of the propellant combustion evolution as possible. Another important point is to estimate the protection material quantity to place between the combustion chamber and the propeller structure. After many methods such as « Strand Burner [1]», ONERA chose ultrasonic techniques whose most interesting feature is their non-intrusivity [2].

Book Title

Review of Progress in Quantitative Nondestructive Evaluation

Volume

16A

Chapter

Chapter 4: NDE Sensors

Section

UT Fields and Probes

Pages

951-958

DOI

10.1007/978-1-4615-5947-4_124

Language

en

File Format

application/pdf

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Jan 1st, 12:00 AM

On a Ray Method for Studying Diffraction of Waves Emitted by a Planar Transducer Within a Solid Conical-Shaped Medium

Brunswick, ME

Increasing rocket engine performance is closely linked to as best a knowledge of the propellant combustion evolution as possible. Another important point is to estimate the protection material quantity to place between the combustion chamber and the propeller structure. After many methods such as « Strand Burner [1]», ONERA chose ultrasonic techniques whose most interesting feature is their non-intrusivity [2].