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Volumn 18, Issue 3, 2002, Pages 641-651

Evaluation of ultrasound technique for solid-propellant burning-rate response measurements

Author keywords

[No Author keywords available]

Indexed keywords

COMBUSTION; DIGITAL SIGNAL PROCESSING; MAGNETIC FLOWMETERS; MATHEMATICAL MODELS; SURFACE ROUGHNESS; ULTRASONIC APPLICATIONS; WAVEFORM ANALYSIS;

EID: 0036575997     PISSN: 07484658     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.5978     Document Type: Article
Times cited : (25)

References (66)
  • 9
    • 0009531862 scopus 로고    scopus 로고
    • Improvements in the measurement of hybrid rocket fuel regression rate using ultrasonic transducers
    • July
    • (1997) AIAA Paper , vol.97 , Issue.3082
    • Leahy, J.C.1    Jackson, J.W.2
  • 23
    • 84987275674 scopus 로고
    • Ultrasonic velocity and attenuation: Measurement methods with scientific and industrial applications
    • edited by W. P. Mason and R. N. Thurston, Academic Press, New York
    • (1976) Physical Acoustics , vol.12 , pp. 277-374
    • Papadakis, E.P.1
  • 47
    • 84999042725 scopus 로고
    • A review of calculations for unsteady burning of solid propellant
    • (1968) AIAA Journal , vol.6 , Issue.12 , pp. 2241-2255
    • Culick, F.E.C.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.