Research objectives and results

Objectives

TSSD concept

The hybrid Laminar Flow Control (HLFC) approach combining optimum wing shape and limited suction, can extend the laminar region on aircraft surfaces such as wings, fin, and fuselage. State of the art of suction panels design is with an internal chambering to provide the chord-specific suction distribution on the outer skin. This leads to a number of constraints between aerodynamic, structural design, and manufacturing. Also, the manufacturing itself is highly complex due to a large number of internal chambers. To simplify the HLFC system, the German Aerospace Center (DLR) has developed a design of suction nose that omits internal chambers, as part of previous works in the Clean Sky 2 research project NACOR (New Innovative Aircraft COnfigurations and Related Issues). The concept is called Tailored Skin Single Duct (TSSD). The TSSD is based on a multilayered tailored outer skin with an intrinsic pressure drop distribution. The outer surface is realized by a micro-perforated metallic foil to ensure a homogeneous control of the boundary layer. By the use of this tailored outer skin, only one internal collector duct with a fixed plenum pressure is necessary.

The ALVAR project: started in Sep 2020 aims at demonstrating a technology readiness level of four for a novel suction skin structure, the tailored skin single duct (TSSD). That is, the technology must be thoroughly tested at representative conditions in a large laboratory. DLR manufactured therefore a suction nose to be tested on a full-scale wind tunnel model of a vertical fin that replicates the surface pressure distribution and Reynolds number of an A320 fin at cruise conditions.

ALVAR project is funded by EU Commission under the CleanSky2 program. It is a collaboration among the Institute of Fluid Mechanics at TU-Braunschweig, the German-Dutch Wind Tunnels (DNW), and the German Aerospace Center, DLR. The experimental campaign was recently held at the large low-speed wind-tunnel facility (LLF) of DNW in The Netherlands.

Results

The experiments of the fin with the TSSD have been carried out in the LLF-DNW in the Netherlands. The model (fin with the TSSD suction panel) was mounted in a test section that has a cross-section of 8 m x 6 m. The maximum speed of 100 m/s was reached. The measurement techniques used are forces balance, pressure measurements, Infrared Thermography, and Particle Image Velocimetry. One of the main objectives of the project is to infer local suction velocities across the suction insert for the first time. The outcomes of the wind-tunnel campaign will be presented in various conferences, and the data will be used for design, validation, and uncertainty analysis.

If successful, the ALVAR project will pave the way for introducing the technology to the wings and tail surfaces of large future commercial aircraft. That could reduce the fuel consumption by 12-15%, with similar savings on the greenhouse effect of the Earth’s atmosphere.

The Fin with the TSSD panel in the LLF-DNW wind-tunnel.
Laminar region and transition on the fin as function of wind speed and plenum pressure.
Laminar region and transition on the fin as function of wind speed and plenum pressure.
ALVAR team with LLF-DNW team.

ALVAR project team

TU-Braunschweig: Prof. Dr.-Ing. Rolf Radespiel, Dr. Camli Badrya, Dr.-Ing. Peter Scholz, Alexander Barklage, M.Sc.

DNW: Dr. Bart van Rooijen

DLR: Dr.-Ing. Arne Seitz, Dr.-Ing. Matthias Horn

DNW-LLF Facility

The Foundation DNW (German-Dutch Wind Tunnels) was established in 1976 by the Dutch National Aerospace Laboratory (NLR) and the German Aerospace Center (DLR), as a non-profit organization under Dutch law. DNW owns the largest low-speed wind tunnel in Europe, the LLF, and operates the aeronautical wind tunnels of DLR and NLR, which are fully integrated with the DNW organization.

Related Publications

TSSD concept design:

Horn, Matthias and Seitz, Arne and Schneider, Marvin, Novel tailored skin single duct concept for HLFC fin application. 7th European Conference for Aeronautics and Space Sciences (EUCASS), 03. - 06. Jul. 2017, Mailand, Italien. doi: 10.13009/EUCASS2017-44.

Uncertainty analysis and quantification of HLFC application on a fin with TSSD suction panel:

Alexander Barklage, Ulrich Romer, Anna Bertram, Philipp Bekemeyer, Jan Himisch, Rolf Radespiel, and Camli Badrya, Analysis and Uncertainty Quantification of a Hybrid Laminar Flow Control System, AIAA SciTech Forum, San-Diego, 2022, DOI: 10.2514/6.2022-2452

Stay tuned for the coming articles, will be presented at the 2022 Aviation Forum meeting:

  1. Wind Tunnel Verification of Laminar Boundary Layer Control TSSD Concept, Arne Seitz; Matthias Horn; Alexander Barklage, Peter Scholz; Camli Badrya; Rolf Radespiel

  2. Uncertainty analysis of the laminar boundary layer control TSSD concept, Alexander Barklage; Ulrich Römer; Arne Seitz; Rolf Radespiel; Peter Scholz; Camli Badrya