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Conceptual Aircraft Design Course

March 23 @ 09:00 - March 27 @ 17:00

A 5-Day Conceptual Aircraft Design Course in collaboration with The German Aerospace Center (DLR) and TU Braunschweig.  March 23-27, 2026.

Venue

The course is hold in ZAL Tech Center:
Hein-Saß-Weg 22
21129 Hamburg, Germany

The lecture room is at DLR, MBSE Lab (Room A-4-130) , 4th floor in the A-Wing.

Tutors

Ingo Staack (TUB)
Björn Nagel (DLR)
Petter Krus (LiU)
Mikael Stenfelt (Saab)
Svjetlana Stekovic (LiU)

Programme

9:00h-10:30 h 11:00h-12:30h 12:30-13:30h 13:30h-15:30h 16:00h-17:30h
Monday Travel to Hamburg (or L00) Welcome lunch buffet Welcome, Introduction to Aircraft Design (L01) Technical Visit ZAL Tech Center
Tuesday Lecture Fundamentals of Aircraft Design (L02) Lecture FAD (L03) Lunch (buffet or canteen) Hands-on exercise (LAB1) & Recap/Task Invited Talk: Airbus Future Projects Office (FPO)
Wednesday Lecture FAD (L04) Lecture FAD (L05) Lunch (buffet or canteen) Talk: Digital Engineering Methods for Aircraft Design at DLR Hands-on exercise (LAB2) & Recap/Task Todo: Evening Activity
Thursday Visit Airbus Factory incl. Final Assembly Line A320 (9:40-11:40) Lunch (buffet or canteen) Lecture FAD (L06) Lecture FAD (L07) Talk: Green Aircraft Design Examples from DLR
Friday Hands-on exercise (LAB3) & Recap/Task & Follow-Up Travel back to Sweden / Lunch individually on the way

Detailed schedule

Course code Topic Responsible person(s) Content/Keywords; Course structure & learning outcomes
L00 Arrival & Registration Leonie, Björn, Ingo Arrival on Sunday evening or Monday morning; Registration; Informal meet and greet; Start with lunch buffet
L01 Introduction to the Course & Aicraft Concept Design (ACD) at a glance Ingo: ACD foundations
Björn: Digital engineering
Petter: Systems engineering
Overview of Aircraft Design Process (Ingo); Requirements definition; Aircraft sizing fundamentals; Importance of normalization (dimensionless coefficients);
References areas & parametar selection (Petter); Parameterisation principles; Data-driven methods (regression, AI) in early design phases
L02 Crash-Course: The Complete Aircraft Design Loop Ingo, Björn Walkthrough of one full conceptual aircraft design cycle (Ingo);
Interdependencies between disciplines (Björn); Trade-offs and iteration logic (Björn);
“On‑the‑fly” treatment of aerodynamics, structures, performance and sizing (Ingo, Björn)
L03 Fundamentals of Lift and Drag Ingo Drag: Aerodynamic forces; Induced drag & parasite drag;
Lift: Lift generation; Lift curve slope; Wing geometry effects; Laminar vs. turbulent flow; Drag polars; Connection to performance & sizing
LAB1 Statistical analysis & Mission calculation
Linking Research Topics to Aircraft Concept Design
Björn, Ingo, Petter Basic statistical methods for design; Mission definition & mission fuel calculation; Performance constraints; How to connect individual research topics to the aircraft design workflow; Data extraction & analysis for conceptual design
L04 Wing Design, Weight Estimation & Structural Engineering (incl. Loads & Stability) Ingo, Mikael, Svjetlana Wing planform geometry (Ingo); High-lift systems (Ingo); Structural integration (Mikael): Initial structural layouts; Weight estimation methods; Center of Gravity (CG) CG and CG-travel (Ingo); Stability and control introduction (Ingo, Mikael); Loads cases and aero-structural interactions (Mikael); Materials & structural performance (Svjetlana)
L05 Mission analysis, Performance Evaluation & Propulsion Fundamentals Ingo, Mikael Mission calculation (Ingo); Performance constraints, sizing diagram (Ingo); Climb/Cruise/loiter performance (Ingo); Propulsion system types & selection criteria (Mikael); Propulsion efficiency; Coupling between propulsion and aerodynamic/mission requirements (Mikael)
LAB2 Drag build-up methods & Digital tools
(OpenVSP, CPACS & TIGL)
Björn, Ingo,Petter Manual drag build‑up; Component drag estimation; Using OpenVSP (import/export workflow); Introduction to CPACS framework; Geometry visualisation with TiGL‑Viewer; Comparison of manual vs. automated methods
L06 Full aircraft configuration from A to Z Ingo, Mikael Fuselage design & sizing (Ingo); Empennage design & tail sizing (Ingo), Engine/propulsion systemintegration (Mikael); Landing gear setups & integration (Ingo);
Special mission influences (e.g., SAR, maritime patrol, research aircraft); Operational considerations & CG management (Ingo)
L07 Systems Engineering: “The devil is in the details” Petter, Ingo, Mikael, Björn, Svjetlana Aircraft systems overview (electric, pneumatic, hydraulic) (Ingo); System integration challenges (Petter, Mikael); Safety and reliability requirements (Ingo); Material-system interactions (Svjetlana)
Future system trends: new system designs and opportunities (Björn)
LAB3 Group formation & Task definition for collaborative projects [examination] Björn, Ingo, Petter Formation of project teams; Definition of project scope; Choosing between e.g. AI‑based individual scripts or collaborative concept design tasks; Development of preliminary project plan; Expectations for the examination submission

Follow-up activities

Follow-up 1 ca. 1 Month after Course Online Catch-up and evt. Specialisation (on Request) (ca. 1h30) Björn, Ingo, Petter
Follow-up 2 ca. 3 Months after Course Onsite Catch-up (e.g. within the SARC annual meeting) to finalize task or collaborative project/paper (ca. 0.5..1.0 day) Björn, Ingo, Petter

Details

  • Start: March 23 @ 09:00
  • End: March 27 @ 17:00
  • Event Category:

Venue

  • DLR Hamburg
  • Hamburg, Germany