مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

video

مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

sound

مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

Persian Version

مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

View:

422
مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

Download:

157
مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

Cites:

Information Journal Paper

Title

AEROSERVOELASTIC BEHAVIOR OF SUPERSONIC GUIDED FLIGHT VEHICLES

Pages

  425-439

Abstract

 Flight dynamics of the guided vehicle is modelled by the aid of linear and angular equations of motions using LAGRANGE'S APPROACH in this paper. Governing equations of the CONTROL SYSTEM and the elastic behavior of the vehicle are added to the equations of dynamic states. Flexibility effect is modelled using the normal modes, GENERALIZED COORDINATES and forces. For validation of modified FORTRAN SIMULATION CODE, the stability of specific vehicles is determined and compared with the same results in the literature.  Using this code and by solving the governing equations for the desired flight vehicle, the AEROSERVOELASTICITY is analyzed and then the results are compared with the rigid cases and with the flight test data. Errors induced to CONTROL SYSTEM sensors are shown in the figures. Good compatibility is achieved between the simulation and the experimental results. Fast Fourier transformations (FFT) is used for extracting the structural flexibility frequencies from the elastic simulation and flight test data.

Cites

  • No record.
  • References

  • No record.
  • Cite

    APA: Copy

    FATHI, M., NOUBARI, A.S., SABZEHPARVAR, M., MOGHADAM, M.M., & HADADPOUR, H.. (2009). AEROSERVOELASTIC BEHAVIOR OF SUPERSONIC GUIDED FLIGHT VEHICLES. IRANIAN JOURNAL OF SCIENCE AND TECHNOLOGY TRANSACTION B- ENGINEERING, 33(B5), 425-439. SID. https://sid.ir/paper/554828/en

    Vancouver: Copy

    FATHI M., NOUBARI A.S., SABZEHPARVAR M., MOGHADAM M.M., HADADPOUR H.. AEROSERVOELASTIC BEHAVIOR OF SUPERSONIC GUIDED FLIGHT VEHICLES. IRANIAN JOURNAL OF SCIENCE AND TECHNOLOGY TRANSACTION B- ENGINEERING[Internet]. 2009;33(B5):425-439. Available from: https://sid.ir/paper/554828/en

    IEEE: Copy

    M. FATHI, A.S. NOUBARI, M. SABZEHPARVAR, M.M. MOGHADAM, and H. HADADPOUR, “AEROSERVOELASTIC BEHAVIOR OF SUPERSONIC GUIDED FLIGHT VEHICLES,” IRANIAN JOURNAL OF SCIENCE AND TECHNOLOGY TRANSACTION B- ENGINEERING, vol. 33, no. B5, pp. 425–439, 2009, [Online]. Available: https://sid.ir/paper/554828/en

    Related Journal Papers

  • No record.
  • Related Seminar Papers

  • No record.
  • Related Plans

  • No record.
  • Recommended Workshops






    Move to top
    telegram sharing button
    whatsapp sharing button
    linkedin sharing button
    twitter sharing button
    email sharing button
    email sharing button
    email sharing button
    sharethis sharing button