Density field of supersonic separated flow past an afterbody nozzle using tomographic reconstruction of BOS data
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- Type
- article
- Published
- 2009-05-23
- Cited by
- 72
- References
- 22
- OpenAlex
- https://openalex.org/W2048790243
- Semantic Scholar
- https://api.semanticscholar.org/CorpusID:121630926
Keywords
Freestream, Schlieren, Jet (fluid), Mechanics, Shock (circulatory)
References
- Effect of fineness ratio on boattail drag of circular-arc afterbodies having closure ratios of 0.50 with jet exhaust at Mach numbers up to 1.30
- Analysis of Unsteadiness in Afterbody Transonic Flows
- Underexpanded jet-freestream interactions on an axisymmetric afterbody configuration
- Whole-field density measurements by ‘synthetic schlieren’
- Density Measurements in an Axisymmetric Underexpanded Jet by Background-Oriented Schlieren Technique
- Effects of Engine Exhaust Flow on Boattail Drag
- Principles of computerized tomographic imaging
- Flow Visualizations and Measurements of a Three-Dimensional Supersonic Separated Flow
- On the applicability of background oriented optical tomography for large scale aerodynamic investigations
- The background oriented schlieren technique: sensitivity, accuracy, resolution and application to a three-dimensional density field
- Flow Confluence Past a Jet-On Axisymmetric Afterbody
- Internal wave excitation by a vertically oscillating elliptical cylinder
- Visualization and measurement of internal waves by ‘synthetic schlieren’. Part 1. Vertically oscillating cylinder
- Drag Reduction from Square-Base Afterbodies at High Speeds
- Three-dimensional schlieren measurements using inverse tomography
- Schlieren measurement of axisymmetric internal wave amplitudes
- Density measurements using the Background Oriented Schlieren technique
- Computerized background-oriented schlieren
- An experimental evaluation of exhaust nozzle/airframe interference
- BOS Density Measurements in Afterbody Flows with Shock and Jet Effects
Cited by
- Image Based Measurement Techniques of Increased Complexity for Industrial Propeller Flow Investigations
- Single camera time-resolved 3D tomographic reconstruction of a pulsed gas jet
- Density Field Measurements of a Supersonic Impinging Jet with Microjet Control
- Reconstruction of the Unsteady Supersonic Flow around a Spike Using the Colored Background Oriented Schlieren Technique
- Improvement in spatial resolution of background-oriented schlieren technique by introducing a telecentric optical system and its application to supersonic flow
- Computed-tomographic density measurement of supersonic flow field by colored-grid background oriented schlieren (CGBOS) technique
- Three-Dimensional Density Measurement of Supersonic and Axisymmetric Flow Field by Colored Grid Background Oriented Schlieren (CGBOS) Technique
- Generation and Control of Oblique Shocks Using Microjets
- Methodology for evaluating hot gas path defects in an exhaust jet
- Review of background oriented schlieren and development for ballistic range applications
- Background-oriented schlieren (BOS) techniques
- Density field visualization of a Micro-explosion using background-oriented schlieren
- COMPARISON BETWEEN CBOS (COLORED BACKGROUND ORIENTED SCHLIEREN) AND CGBOS (COLORED-GRID BACKGROUND ORIENTED SCHLIEREN) FOR SUPERSONIC FLOW
- VELOCITY AND DENSITY FIELD MEASUREMENTS OF A MICRO- EXPLOSION
- Development of 3D Background Oriented Schlieren with a Plenoptic Camera
- A direct approach for instantaneous 3D density field reconstruction from background-oriented schlieren (BOS) measurements
- Quantitative Visualization of Vortices Discharged from Open-end of Shock Tube Using Background-Oriented Schlieren Method
- Three-dimensional Density Measurement and Reconstruction of Asymmetric Flow Field by Colored Grid Background Oriented Schlieren (CGBOS) Technique
- Recent Developments in Schlieren and Shadowgraphy
- Tomographic schlieren system for visualisation of supersonic jet
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