Search Publications
Refine Results
Filter By Date
Filter By Type
Filter By IsPartOf
- Aerodynamic Decelerator Systems Technology Conferences (1)
- Aerospace Sciences Meetings (7)
- AIAA AVIATION Forum (6)
- AIAA Journal (2)
- AIAA SciTech Forum (4)
- Fluid Dynamics and Co-located Conferences (4)
- Joint Propulsion Conferences (2)
- Journal of Spacecraft and Rockets (1)
- Journal of Thermophysics and Heat Transfer (1)
-
Stability Analysis of HIFiRE 1 with Flight Wall Temperatures
Laminar to turbulent boundary layer transition is sensitive to wall temperature distribution and freestream disturbances. The wall temperature can increase the boundary layer thickness and affect the growth rate of disturbances in the boundary layer. ...
- Flow Control of Swept Fin Shock Interactions by Laser-Induced Plasmas
- Geometric Effects on the Amplification of First Mode Instability Waves
- DNS of Transition To Turbulence in a Mach 6 Boundary Layer
- Simulation of ram-accelerator flowfields using elemental conservation equations
- DNS of transition to turbulence in a hypersonic boundary layer
- Hypersonic Inward Turning Inlets: Design and Optimization
- Computational Simulation of Laser-Induced Plasmas for Supersonic Flow Control
- Numerical study of shock interactions on double-wedge geometries
-
Computing Measured Spectra from Hypersonic Pitot Probes with Flow-Parallel Freestream Disturbances
December 01, 2017
The relationship between freestream disturbances and measured pitot pressure spectra, defined as the transfer function, is investigated. Pitot probes used to characterize hypersonic facilities are considered for a variety of freestream conditions and flow-... -
Characterization of Freestream Disturbances in Conventional Hypersonic Wind Tunnels
March 01, 2019
Although low-disturbance (“quiet”) hypersonic wind tunnels are believed to provide more reliable extrapolation of boundary-layer transition behavior from ground to flight, the presently available quiet facilities are limited to Mach 6, moderate Reynolds ... - Simulation of Injection Into a Supersonic Crossflow using DES with Synthetic Inflow
- Input-output analysis of complex hypersonic boundary layers
- Recovery of Freestream Acoustic Disturbances from Stagnation Pressure Spectrum in Hypersonic Flow
- Detached Eddy Simulations of Flush Wall Injection into a Supersonic Freestream
- DES Investigation of Transverse Injection into Supersonic Crossflow using a Hybrid Unstructured Solver
- Hypersonic Transition to Turbulence Triggered by Isolated Roughness Elements
- Direct numerical simulation of BOLT hypersonic flight vehicle
- A Synthetic Inflow Generation Method Using the Attached Eddy Hypothesis
-
Numerical Simulation of Gas Flow over Microscale Airfoils
April 01, 2002