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Volumn 14, Issue 2, 1998, Pages 241-246

Aerodynamics performance prediction of thrust-vectoring nozzles

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; DEGREES OF FREEDOM (MECHANICS); FIGHTER AIRCRAFT; NUMERICAL ANALYSIS; THRUST REVERSAL;

EID: 0032023175     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/2.5273     Document Type: Article
Times cited : (10)

References (19)
  • 2
    • 0029778690 scopus 로고    scopus 로고
    • X-31 a Quasi-Tailless Evaluation
    • Inst. of Electrical and Electronics Engineers, New York
    • Loria, C. J., Kelly, M., and Hatney, R., "X-31 A Quasi-Tailless Evaluation," IEEE Aerospace Applications Conference; Inst. of Electrical and Electronics Engineers, Vol. 4, New York, 1996, pp. 253-276.
    • (1996) IEEE Aerospace Applications Conference , vol.4 , pp. 253-276
    • Loria, C.J.1    Kelly, M.2    Hatney, R.3
  • 3
    • 79952800792 scopus 로고
    • Performance Characteristics of a Variable-Area Vane Nozzle for Vectoring an ASTOVL Exhaust Jet up to 45 Degrees
    • June
    • Macardle, J. G., and Esker, B. S., "Performance Characteristics of a Variable-Area Vane Nozzle for Vectoring an ASTOVL Exhaust Jet up to 45 Degrees," AIAA Paper 93-2437, June 1993.
    • (1993) AIAA Paper 93-2437
    • Macardle, J.G.1    Esker, B.S.2
  • 4
    • 84889204912 scopus 로고
    • Static Internal Performance Including Thrust Vectoring and Reversing of Two-Dimensional Convergent-Divergent Nozzles
    • Feb.
    • Re, R. J., and Leavitt, L. D., "Static Internal Performance Including Thrust Vectoring and Reversing of Two-Dimensional Convergent-Divergent Nozzles," NASA TP-2253, Feb. 1984.
    • (1984) NASA TP-2253
    • Re, R.J.1    Leavitt, L.D.2
  • 5
    • 84889205423 scopus 로고
    • Static Investigation of a Two-Dimensional Convergent-Divergent Exhaust Nozzle with Multiaxis Thrust-Vectoring Capability
    • April
    • Taylor, J. G., "Static Investigation of a Two-Dimensional Convergent-Divergent Exhaust Nozzle with Multiaxis Thrust-Vectoring Capability," NASA TP-2973, April 1990.
    • (1990) NASA TP-2973
    • Taylor, J.G.1
  • 6
    • 85081466265 scopus 로고
    • Scale Model Test Results for Several Spherical Two-Dimensional Nozzle Concepts
    • June
    • Maclean, M. K., and Meyer, B. E., "Scale Model Test Results for Several Spherical Two-Dimensional Nozzle Concepts," AIAA Paper 93-2430, June 1993.
    • (1993) AIAA Paper 93-2430
    • Maclean, M.K.1    Meyer, B.E.2
  • 7
    • 85081471234 scopus 로고
    • Experimental Investigation of Spherical Convergent-Flap Thrust-Vectoring Two-Dimensional Plug Nozzle
    • June
    • Cler, D. L., Mason, M. L., and Guthrie, A. R., "Experimental Investigation of Spherical Convergent-Flap Thrust-Vectoring Two-Dimensional Plug Nozzle," AIAA Paper 93-2431, June 1993.
    • (1993) AIAA Paper 93-2431
    • Cler, D.L.1    Mason, M.L.2    Guthrie, A.R.3
  • 8
    • 85081463331 scopus 로고
    • Numerical Study on Some Fluid Dynamics Aspects of Axisymmetric Thrust Vectoring Nozzles
    • June
    • Matesanz, A., Velázquez, A., and Rodríguez, M., "Numerical Study on Some Fluid Dynamics Aspects of Axisymmetric Thrust Vectoring Nozzles," AIAA Paper 94-3365, June 1994.
    • (1994) AIAA Paper 94-3365
    • Matesanz, A.1    Velázquez, A.2    Rodríguez, M.3
  • 9
    • 0005860523 scopus 로고
    • Static Internal Performance of an Axisymmetric Nozzle with Multiaxis Thrust-Vectoring Capability
    • Feb.
    • Carson, G. T., and Capone, F. J., "Static Internal Performance of an Axisymmetric Nozzle with Multiaxis Thrust-Vectoring Capability," NASA TM-4237, Feb. 1991.
    • (1991) NASA TM-4237
    • Carson, G.T.1    Capone, F.J.2
  • 10
    • 84964450539 scopus 로고
    • Performance Characteristics of Two Multiaxis Thrust-Vectoring Nozzles at Mach Number up to 1.28
    • May
    • Wing, D. J., "Performance Characteristics of Two Multiaxis Thrust-Vectoring Nozzles at Mach Number up to 1.28," NASA TP-3313, May 1993.
    • (1993) NASA TP-3313
    • Wing, D.J.1
  • 11
    • 0028259889 scopus 로고
    • Numerical Study of Unsteady Supersonic Compression Ramp Flows
    • Park, S. O., Chung, Y. M., and Sung, H. J., "Numerical Study of Unsteady Supersonic Compression Ramp Flows," AIAA Journal, Vol. 32, No. 1, 1994, pp. 216-218.
    • (1994) AIAA Journal , vol.32 , Issue.1 , pp. 216-218
    • Park, S.O.1    Chung, Y.M.2    Sung, H.J.3
  • 13
    • 0021497923 scopus 로고
    • Finite Element Methods for First-Order Hyperbolic Systems with Particular Emphasis on the Compressible Euler Equations
    • Hughes, T. J. R., and Tezduyar, T. E., "Finite Element Methods for First-Order Hyperbolic Systems with Particular Emphasis on the Compressible Euler Equations," Computer Methods in Applied Mechanics and Engineering, Vol. 45, 1984, pp. 217-284.
    • (1984) Computer Methods in Applied Mechanics and Engineering , vol.45 , pp. 217-284
    • Hughes, T.J.R.1    Tezduyar, T.E.2
  • 14
    • 84997751496 scopus 로고
    • Mach Disk Simulation in Jets from Convergent-Divergent Axisymmetric and Thrust Vectoring Nozzles
    • June
    • Matesanz, A., Velázquez, A., and Rodriguez, M., "Mach Disk Simulation in Jets from Convergent-Divergent Axisymmetric and Thrust Vectoring Nozzles," AIAA Paper 94-2328, June 1994.
    • (1994) AIAA Paper 94-2328
    • Matesanz, A.1    Velázquez, A.2    Rodriguez, M.3
  • 15
    • 0344311451 scopus 로고
    • Numerical Simulation of Slot Film Cooling in Convergent-Divergent Nozzles
    • June
    • Matesanz, A., Velázquez, A., and Rodriguez, M., "Numerical Simulation of Slot Film Cooling in Convergent-Divergent Nozzles," AIAA Paper 93-1977, June 1993.
    • (1993) AIAA Paper 93-1977
    • Matesanz, A.1    Velázquez, A.2    Rodriguez, M.3
  • 18
    • 5244264052 scopus 로고
    • Effect on Gaseous Film Cooling of Coolant Injection Through Angled Slots and Normal Holes
    • Sept.
    • Papell, S., "Effect on Gaseous Film Cooling of Coolant Injection Through Angled Slots and Normal Holes," NASA TN D-299, Sept. 1960.
    • (1960) NASA TN D-299
    • Papell, S.1
  • 19
    • 0019354196 scopus 로고
    • Effect of Axisymmetric Sonic Nozzle Geometry on Mach Disk Characteristics
    • Addy, A. L., "Effect of Axisymmetric Sonic Nozzle Geometry on Mach Disk Characteristics," AIAA Journal, Vol. 19, No. 1, 1981, p. 121.
    • (1981) AIAA Journal , vol.19 , Issue.1 , pp. 121
    • Addy, A.L.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.