Airframe Integration

Airframe Integration is a design methodology that systematically couples the aerodynamic, structural, and propulsion systems of a hypersonic vehicle to achieve optimized performance by ensuring mutual compatibility and synergistic interaction between the airframe and the scramjet engine.

264

Publications

10.3K

Citations

697

Authors

153

Institutions

Publications per year

2017–2026

46

Variants

Airframe-propulsion Integration

Authors

697

  1. ML
    Mark Lewis

    University of Maryland, College Park, United States

    10 publications · 399 citations

    10

    h-index

  2. WC
    Walter C. Engelund

    Langley Research Center, United States

    6 publications · 178 citations

    6

    h-index

  3. CR
    Charles R. McClinton

    Langley Research Center, United States

    6 publications · 175 citations

    6

    h-index

  4. DN
    Dimitri N. Mavris

    Georgia Institute of Technology, United States

    5 publications · 221 citations

    5

    h-index

  5. AS
    Arne Seitz

    Bauhaus Luftfahrt, Germany

    5 publications · 145 citations

    5

    h-index

1–5 of 697

Venues

  1. Journal of Aircraft

    26 publications · 960 citations

    17

    h-index

  2. NASA Technical Reports Server (NASA)

    Repository · 14 publications · 315 citations

    12

    h-index

  3. Journal of Propulsion and Power

    13 publications · 482 citations

    11

    h-index

  4. Journal of Spacecraft and Rockets

    9 publications · 278 citations

    9

    h-index

  5. Aerospace Science and Technology

    AST · 7 publications · 270 citations

    7

    h-index

1–5