Stability Configuration

Stability Configuration is a method within the field of aircraft configuration design that systematically integrates aerodynamic, inertial, and control surface parameters to achieve desired static and dynamic stability characteristics in an aircraft’s flight envelope.

6

Publications

131

Citations

16

Authors

6

Institutions

Publications per year

2017–2026

3

Authors

16

  1. GM
    Galal M. Moatimid

    Ain Shams University, Egypt

    2 publications · 50 citations

    2

    h-index

  2. KJ
    Kyle J. Hovey

    John Carroll University, United States

    1 publications · 27 citations

    1

    h-index

  3. PS
    Paul S. Shamble

    Harvard University Press, United States

    1 publications · 27 citations

    1

    h-index

  4. TL
    Thomas Loeser

    Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR), Germany

    1 publications · 17 citations

    1

    h-index

  5. CH
    C H Zimmerman

    The University of Texas at Austin, United States

    1 publications · 15 citations

    1

    h-index

1–5 of 16

Venues

  1. 2

    h-index

  2. Journal of Experimental Biology

    1 publications · 27 citations

    1

    h-index

  3. Arabian Journal for Science and Engineering

    1 publications · 33 citations

    1

    h-index

  4. DOAJ (DOAJ: Directory of Open Access Journals)

    Repository · 1 publications · 17 citations

    1

    h-index

1–4