Hypersonic Vehicle Analyses: The Needs and Challenges of Multidisciplinary Simulations - presented by Prof. Iain Boyd

Hypersonic Vehicle Analyses: The Needs and Challenges of Multidisciplinary Simulations

Prof. Iain Boyd

Prof. Iain Boyd
Slide at 09:01
CENTER FOR
NATIONAL
Hypersonic Vehicle Analyses:
SECURITY INITIATIVES
Research Needs
High fidelity predictive models of each sub-system Reliable multidisciplinary analysis approaches
Ablating Capsule
Deforming Hot Structure
Before entry
After entry
Propulsion-airframe integrated scramjet
Forebody
Shock boundary
compression
Aftbody
layer interactions
expansion
1.26
14.6 cm
10cm
meters
Airflow
Vehicle
bow shock
Fuel injection stages
Inlet
Isolator
Combustor
Nozzle
- Hot flow ablates vehicle surface
- Hot flow heats, deforms structure
- Shape change alters aerodynamics
- Deformation alters engine inlet
- Aerodynamics affects GNC
- Inlet controls scramjet performance
- Need: Coupled analysis of flow,
- Need: Coupled analysis of flow,
materials, and GNC to take
structure, and propulsion, to
advantage of shape change
maximize system performance
University of Colorado
Boulder
Be Boulder.
Share slide
Summary (AI generated)

Here are two examples to consider. On the left side, there is an example from space exploration. The black outline with the red cursor represents a heat shield on a capsule entering a planet's atmosphere. As the capsule experiences high temperatures, a large portion of the heat shield is intentionally ablated away. The gold area on the right side shows a prediction of the amount of heat shield removed. During hypersonic entry, the vehicle encounters high temperatures, causing ablation of the material surface and a change in the vehicle's shape, affecting aerodynamic coefficients.

On the right side is a Scramjet example. A Scramjet is an engine used for Hypersonic vehicles. The diagram shows the tight coupling between fluid mechanics, aerothermodynamics, and vehicle shape. The front of the vehicle is designed to create shock waves that condition the air for combustion in the Scramjet. The heated air affects the structure's integrity, potentially changing the vehicle's shape and performance. Understanding these processes requires modeling flow, material response, structure response, and propulsion system simultaneously. This integration is essential for optimizing vehicle performance. Today, I will discuss the progress we have made in this area at our Colorado facility.