Showing 1 - 20 results of 88 for search '', query time: 0.23s Refine Results
  1. 1
    Finite difference time marching in the frequency domain : a parabolic formulation for aircraft acoustic nacelle design /
    by Baumeister, Kenneth J
    Published 1996

    Government Document Book
  2. 2
    Investigation of "6X" scramjet inlet configurations /

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    Government Document Book
  3. 3
    Mach 10 experimental database of a three-dimensional scramjet inlet flow field /

    Government Document Book
  4. 4
    Improved NASA-ANOPP noise prediction computer code for advanced subsonic propulsion systems
    Published 1996

    Government Document Book
  5. 5
    Flow through a rectangular-to-semiannular diffusing transition duct
    Published 1997

    Government Document Book
  6. 6
    IPAC--Inlet Performance Analysis Code
    by Barnhart, Paul J
    Published 1997

    Government Document Book
  7. 7
    Fan noise prediction system development source/radiation field coupling and workstation conversion for the acoustic radiation code /
    by Meyer, H. D
    Published 1993

    Government Document Book
  8. 8
    Improved finite element modeling of the turbofan engine inlet radiation problem
    by Roy, Indranil Danda
    Published 1993

    Government Document Book
  9. 9
    Fan noise prediction assessment
    by Bent, Paul H
    Published 1995

    Government Document Book
  10. 10
    3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
    by Mizukami, M
    Published 1995

    Government Document Book
  11. 11
    PARC3D calculations of the F/A-18A HARV inlet vortex generators
    by Podleski, Steve D
    Published 1995

    Government Document Book
  12. 12
    Time-dependent parabolic finite difference formulation for harmonic sound propagation in a two-dimensional duct with flow /
    by Baumeister, Kenneth J
    Published 1996

    Government Document Book
  13. 13
    Comparison of the aeroacoustics of two small-scale supersonic inlets final technical report, NASA contract #--NAG 3-1539 /
    by Ng, Wing
    Published 1996

    Government Document Book
  14. 14
    Development of a low-Reynolds number, nonlinear [kappa-epsilon] model for the reduced Navier-Stokes equations a final technical report for NASA-LeRC grant NAG-1781 /
    by Boger, David A
    Published 1997

    Government Document Book
  15. 15
    Dynamic inlet distortion prediction with a combined computational fluid dynamics and distortion synthesis approach
    by Norby, W. P
    Published 1996

    Government Document Book
  16. 16
    Evaluation of panel code predictions with experimental results of inlet performance for a 17-inch ducted prop/fan simulator operating at mach 0.2
    Published 1991

    Government Document Book
  17. 17
    NASA Lewis Propulsion Systems Laboratory customer guide manual
    by Soeder, Ronald H
    Published 1994

    Government Document Book
  18. 18
    Final technical report on grant NAG3-1567 entitled Inlet distortion in engines on VSTOL aircraft
    by Tan, Choon Sooi
    Published 1994

    Government Document Book
  19. 19
    Prediction of wind tunnel effects on the installed F/A-18A inlet flow field at high angles-of-attack
    by Smith, Crawford F
    Published 1995

    Government Document Book
  20. 20
    Collection efficiency and ice accretion calculations for a sphere, a swept MS(1)-317 wing, a swept NACA-0012 wing tip, an axisymmetric inlet, and a Boeing 737-300 inlet
    by Bidwell, Colin S
    Published 1995

    Government Document Book
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