Capacitive Vector Skin Friction Measurement Systems for Complex Flow Fields, Phase I

The Interdisciplinary Consulting Corporation (IC2) proposes to develop dual-axis shear stress sensors that are applicable in ground test facilities covering a large range of flow speeds in response to NASA SBIR 2018 Phase I solicitation subtopic A1.08: Aeronautics Ground Test and Measurements Technologies. The proposed sensing system addresses a critically unmet measurement need in NASA’s technology portfolio, specifically the ability to make time-resolved, continuous, direct, two-dimensional measurements of mean and fluctuating wall shear stress in wall-bounded turbulent and transitional flows in subsonic and transonic facilities. The realization of this capability not only benefits advanced air vehicle development but also impacts fundamental compressible boundary layer physics research areas such as transition to turbulence in three-dimensional flows, extending the current capabilities of NASA’s ground test facilities.

The proposed innovation is a dual-axis, instrumentation-grade, robust, high-bandwidth, high-resolution, silicon micromachined differential capacitive shear stress sensor for subsonic and transonic applications. The sensor system will enable localized, non-intrusive, vector measurement of mean and fluctuating wall shear stress for characterization of complex boundary-layer flows in ground-test facilities. The differential capacitive measurement scheme offers high sensitivity to in-plane shear stress as well as common-mode rejection of pressure fluctuations. Two sets of differential capacitors provide shear stress measurement capability in two orthogonal directions to provide the wall shear stress vector. Backside electrical contacts using IC2’s patent-pending fabrication and packaging process enable the sensor to remain flush with the test article surface while significantly reducing fabrication complexity and cost. The modeling aspects of the proposed design approach facilitate design optimization for various applications and flow conditions.

Data and Resources

Field Value
accessLevel public
bureauCode {026:00}
catalog_@context https://project-open-data.cio.gov/v1.1/schema/catalog.jsonld
catalog_@id https://data.nasa.gov/data.json
catalog_conformsTo https://project-open-data.cio.gov/v1.1/schema
catalog_describedBy https://project-open-data.cio.gov/v1.1/schema/catalog.json
identifier TECHPORT_94520
issued 2019-01-01
landingPage https://techport.nasa.gov/view/94520
modified 2020-01-29
programCode {026:027}
publisher Space Technology Mission Directorate
resource-type Dataset
source_datajson_identifier true
source_hash a67619542364f69d03a65c6adfc5963ecf2ff74c
source_schema_version 1.1
Groups
  • AmeriGEOSS
  • National Provider
  • North America
Tags
  • active
  • amerigeo
  • amerigeoss
  • ckan
  • geo
  • geoss
  • langley-research-center
  • national
  • north-america
  • united-states
isopen False
license_id notspecified
license_title License not specified
maintainer TECHPORT SUPPORT
maintainer_email hq-techport@mail.nasa.gov
metadata_created 2025-11-23T00:22:16.071498
metadata_modified 2025-11-23T00:22:16.071502
notes <p style="margin-left:0in; margin-right:0in">The Interdisciplinary Consulting Corporation (IC<sup>2</sup>) proposes to develop dual-axis shear stress sensors that are applicable in ground test facilities covering a large range of flow speeds in response to NASA SBIR 2018 Phase I solicitation subtopic <em>A1.08: Aeronautics Ground Test and Measurements Technologies</em>.&nbsp;The proposed sensing system addresses a critically unmet measurement need in NASA&rsquo;s technology portfolio, specifically the ability to make time-resolved, continuous, direct, two-dimensional measurements of mean and fluctuating wall shear stress in wall-bounded turbulent and transitional flows in subsonic and transonic facilities.&nbsp;The realization of this capability not only benefits advanced air vehicle development but also impacts fundamental compressible boundary layer physics research areas such as transition to turbulence in three-dimensional flows, extending the current capabilities of NASA&rsquo;s ground test facilities.</p> <p style="margin-left:0in; margin-right:0in">The proposed innovation is a dual-axis, instrumentation-grade, robust, high-bandwidth, high-resolution, silicon micromachined differential capacitive shear stress sensor for subsonic and transonic applications.&nbsp;The sensor system will enable localized, <strong>non-intrusive, vector measurement of mean and fluctuating wall shear stress</strong> for characterization of complex boundary-layer flows in ground-test facilities.&nbsp;The differential capacitive measurement scheme offers high sensitivity to in-plane shear stress as well as common-mode rejection of pressure fluctuations.&nbsp;Two sets of differential capacitors provide shear stress measurement capability in two orthogonal directions to provide the wall shear stress vector.&nbsp;Backside electrical contacts using IC<sup>2</sup>&rsquo;s patent-pending fabrication and packaging process enable the sensor to remain flush with the test article surface while significantly reducing fabrication complexity and cost.&nbsp;The modeling aspects of the proposed design approach facilitate design optimization for various applications and flow conditions.</p>
num_resources 4
num_tags 10
title Capacitive Vector Skin Friction Measurement Systems for Complex Flow Fields, Phase I