Flight Envelope Loads

Flight Envelope Loads is a structural and aerodynamic load construct that characterizes the extreme and operational forces acting on an aircraft across its entire permissible range of altitude, speed, and maneuver conditions within the flight envelope.

14

Publications

370

Citations

46

Authors

16

Institutions

Publications per year

2017–2026

5

Authors

46

  1. SS
    Sven Schmitz

    Pennsylvania State University, United States

    1 publications · 14 citations

    1

    h-index

  2. PM
    Pierangelo Masarati

    Politecnico di Milano, Italy

    1 publications · 25 citations

    1

    h-index

  3. TJ
    T. J. Gregory

    Ames Research Center, United States

    1 publications · 11 citations

    1

    h-index

  4. MN
    Martin Neubauer

    University of Bayreuth, Germany

    1 publications · 12 citations

    1

    h-index

  5. DF
    Dario Floreano

    École Polytechnique Fédérale de Lausanne, Switzerland

    1 publications · 86 citations

    1

    h-index

1–5 of 46

Venues

  1. Journal of Aircraft

    4 publications · 63 citations

    4

    h-index

  2. IEEE Robotics and Automation Letters

    1 publications · 86 citations

    1

    h-index

  3. The Aeronautical Journal

    1 publications · 33 citations

    1

    h-index

  4. 54th AIAA Aerospace Sciences Meeting

    1 publications · 24 citations

    1

    h-index

  5. 1

    h-index

1–5