CompletedAerospacePhysics

DLR (German Aerospace Center) Internship

Hypersonic aerodynamics and scramjet testing at Mach 10

RoleIntern
TimelineApr–May 2022
Duration1 week
FacilityDLR hypersonic wind tunnel
Test SpeedMach 10
Optical instruments aligned on a laboratory rail at the German Aerospace Center
3D-printed aerospace component mounted in a DLR test rig
Electronics and breadboard experiment on a DLR workbench
Overview

I spent one week at DLR (German Aerospace Center) in the hypersonic wind-tunnel facility. Under supervision, I worked with Mach 10 test equipment, calculated airfoil efficiency at hypersonic speeds, and examined scramjet-combustor aerodynamics data. Most of the week alternated between tests, calculations, and engineers explaining what the measurements meant.


The problem

Get meaningful technical understanding out of one week in a world-class hypersonic research facility.

Constraints
  • One-week duration, which required being selective about what was worth focusing on
  • Test facility safety protocols limited hands-on equipment operation to supervised sessions
Design decisions
  • Spent most of the available time on aerodynamic analysis, where my existing physics background let me understand and contribute more within a one-week placement.
Build process
  1. 01

    Wind tunnel facility orientation and safety protocol certification

  2. 02

    Mach 10 airfoil testing: data collection and drag/lift coefficient analysis across multiple geometries

  3. 03

    Scramjet combustor aerodynamics: inlet and flow path efficiency analysis


Result

Calculated efficiency curves for several airfoil geometries at Mach 10. Documented scramjet inlet aerodynamics analysis.

What went wrong / what I learned
  • Hypersonic aerodynamics has almost nothing in common with subsonic intuition. Shock interactions and aerodynamic heating dominate everything.
  • High-end research facilities spend more time on calibration and diagnostics than on actual test runs

Tools & Methods

Hypersonic wind tunnel instrumentationAerodynamic analysisCFD diagnostics

Specs

Duration
1 week
Facility
DLR hypersonic wind tunnel
Test Speed
Mach 10