메뉴 건너뛰기




Volumn , Issue , 1996, Pages 1-12

Quantification of data uncertainties and validation of cfd results in the development of hypersonic airbreathing engines

Author keywords

[No Author keywords available]

Indexed keywords

ENGINES; FLUID DYNAMICS;

EID: 84959215794     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (3)

References (17)
  • 1
    • 5244266816 scopus 로고
    • Guide to Credible Computational Fluid Dynamic Simulations
    • Jun
    • Mehta, U. B., Guide to Credible Computational Fluid Dynamic Simulations, AIAA 95-2225, (Jun 1995).
    • (1995) AIAA 95-2225
    • Mehta, U.B.1
  • 2
    • 84959220518 scopus 로고
    • Comparison of Hypersonic Ramjet Engines with Supersonic and Subsonic Combustion
    • Milan, Italy, Apr
    • Dugger, G. L., Comparison of Hypersonic Ramjet Engines with Supersonic and Subsonic Combustion, Fourth AGARD Combustion and Propulsion Colloquium, Milan, Italy, (Apr 1960).
    • (1960) Fourth AGARD Combustion and Propulsion Colloquium
    • Dugger, G.L.1
  • 3
    • 84959246675 scopus 로고
    • Possible Directions of Future Research in Airbreathing Engines
    • Milan, Italy, Apr
    • Ferri, A., Possible Directions of Future Research in Airbreathing Engines, Fourth AGARD Combustion and Propulsion Colloquium, Milan, Italy, (Apr 1960).
    • (1960) Fourth AGARD Combustion and Propulsion Colloquium
    • Ferri, A.1
  • 6
    • 0023406468 scopus 로고
    • Evolution and Application of CFD Techniques for Scramjet Engine Analysis
    • Sept-Oct
    • White, M. E., Drummond, J. P., and Kumar, A., “Evolution and Application of CFD Techniques for Scramjet Engine Analysis,” J. Propulsion and Power, 3(5), 423-439 (Sept-Oct 1987).
    • (1987) J. Propulsion and Power , vol.3 , Issue.5 , pp. 423-439
    • White, M.E.1    Drummond, J.P.2    Kumar, A.3
  • 10
  • 11
    • 85003268455 scopus 로고
    • Hypersonic Inlet Performance from Direct Force Measurements
    • Mar-Apr
    • Kutschenreuter, P. H., and Balent, R. L., “Hypersonic Inlet Performance from Direct Force Measurements,” J. Spacecraft, 2 (2) 5 (Mar-Apr 1965).
    • (1965) J. Spacecraft , vol.2 , Issue.2 , pp. 5
    • Kutschenreuter, P.H.1    Balent, R.L.2
  • 15
    • 0028464190 scopus 로고
    • Experimental and Computational Results for the External Flowfield of a Scramjet Inlet
    • Jul-Aug
    • Ault, D. A., and Van Wie, D. M., “Experimental and Computational Results for the External Flowfield of a Scramjet Inlet,” J. Propulsion and Power, 10 (4). 533-539 1994 (Jul-Aug 1994).
    • (1994) J. Propulsion and Power , vol.10 , Issue.4 , pp. 533-539
    • Ault, D.A.1    Van Wie, D.M.2
  • 16
    • 0029679387 scopus 로고    scopus 로고
    • Internal Flowfield Characteristics of a Scramjet Inlet at Mach 10
    • Jan-Feb
    • Van Wie, D. M., and Ault, D. A., “Internal Flowfield Characteristics of a Scramjet Inlet at Mach 10,” J. Propulsion and Power, 12 (1), 158-164 (Jan-Feb 1996).
    • (1996) J. Propulsion and Power , vol.12 , Issue.1 , pp. 158-164
    • Van Wie, D.M.1    Ault, D.A.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.