Angle Of Attack Effects

Angle of Attack Effects is a theoretical construct in aerodynamics that denotes the causal relationship between the angle formed by the chord line of an airfoil and the relative wind direction, and the resulting aerodynamic forces and moments, particularly lift and flow separation characteristics, which determine stall onset and post-stall behavior.

350

Publications

10.7K

Citations

816

Authors

271

Institutions

Publications per year

2017–2026

59

Authors

816

  1. ER
    E. R. Keener

    Ames Research Center, United States

    7 publications · 358 citations

    7

    h-index

  2. SB
    S. B. Grafton

    Langley Research Center, United States

    6 publications · 140 citations

    6

    h-index

  3. GT
    G. T. Chapman

    Ames Research Center, United States

    6 publications · 302 citations

    6

    h-index

  4. BŞ
    Beşi̇r Şahi̇n

    Cukurova University, Türkiye

    6 publications · 131 citations

    6

    h-index

  5. RM
    Robert M. Hall

    Langley Research Center, United States

    5 publications · 129 citations

    5

    h-index

1–5 of 816

Venues

  1. Journal of Aircraft

    45 publications · 1.4K citations

    21

    h-index

  2. AIAA Journal

    28 publications · 1K citations

    19

    h-index

  3. NASA Technical Reports Server (NASA)

    Repository · 21 publications · 482 citations

    13

    h-index

  4. University of North Texas Digital Library (University of North Texas)

    Repository · 12 publications · 334 citations

    12

    h-index

  5. NASA STI Repository (National Aeronautics and Space Administration)

    Repository · 14 publications · 265 citations

    11

    h-index

1–5