skip to content

NASA Logo

Langley Research Center

Turbulence Modeling Resource

 

Exp: Sandia Axisymmetric Transonic Bump (revisiting Bachalo-Johnson)

Return to: Data from Experiments - Intro Page

Return to: Turbulence Modeling Resource Home Page


 

The information on this page was provided by Matthew Barone.

Sandia National Labs undertook to experimentally revisit the classic Bachalo-Johnson axisymmetric transonic bump experiment (see: ATB: Axisymmetric Transonic Bump). This constitutes an experimental characterization of transonic, turbulent, separated flow generated by an axisymmetric model. The test case was also issued as a "CFD challenge."

The model is a scaled version of the geometry in Bachalo and Johnson, AIAA J. (1986), consisting of a circular bump on a constant-diameter cylinder aligned with the flow. The flow is turbulent approaching the hump and becomes locally supersonic at the apex. This leads to a shock-wave/boundary-layer interaction, a turbulent separation bubble, and flow reattachment downstream. Tunnel boundary conditions are characterized and mean surface pressure, mean skin friction, and both mean and fluctuating velocity fields are measured throughout the interaction region. Documentation can be found in (the first journal artricle reference supercedes the earlier AIAA papers):


 

Photo 1 of the axisymmetric transonic hump model installed into Sandia’s Trisonic Wind Tunnel

Photo 2 of the axisymmetric transonic hump model installed into Sandia’s Trisonic Wind Tunnel Photo 3 of the axisymmetric transonic hump model installed into Sandia’s Trisonic Wind Tunnel


 

Details about the experimental data can be found in the first reference listed above. The following table (taken from the reference) lists the tunnel boundary conditions. Rows in grey correspond to derived quantities that should be used for reference only.

Table of boundary conditions, from AIAA-2020-1309

The experimental data are provided in the following file:


 

Return to: Data from Experiments - Intro Page

Return to: Turbulence Modeling Resource Home Page


 
 


Recent significant updates:
02/21/2025 - Added latest journal article reference

Privacy Act Statement

Accessibility Statement

Responsible NASA Official: Ethan Vogel
Page Curator: Clark Pederson
Last Updated: 04/08/2025