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Download Project Report: |
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PERSISTENT IDENTIFIER: | |
URN: | https://nbn-resolving.org/urn:nbn:de:gbv:18302-aero2021-03-30.017 (to reach this page) |
DOI: | https://doi.org/10.15488/11556 |
ARK: | https://n2t.net/ark:/13960/s2dm83bk1d4 |
Associated research data: | https://doi.org/10.7910/DVN/UK2SIV (Excel File and User Guide) |
Alternatively Read in English: |
TORENBEEK:
Synthesis of Subsonic Airplane Design (PDF, 100 MB)
E-4.2 (p.473) "Spawise Lift Distribution" and E-4.4 (p. 475) "Maximum Lift".
Source: "Diederich Method" (NACA). ![]() |
Download User Guide: |
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Download Excel File: |
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Prof. Dr. Scholz
Aircraft Design and Systems Group (AERO)
Aeronautical Engineering
Department of Automotive and Aeronautical Engineering
Faculty of Engineering and Computer Science
Hamburg University of Applied Sciences