A study of moderately underexpanded single and twinjet rocket exhaust plumes in quiescent and in a mach 7 hypersonic freestream

A study of moderately underexpanded single and twinjet rocket exhaust plumes in quiescent and in a mach 7 hypersonic freestream

Rocket plume flowfields have an importance due to their influence on the signature of the rocket and also on the distribution of the plume gases around the vehicle. Little information on the co-flowing situation exists other than a previous study at Oxford. This thesis thus represents a significant...

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Bibliografiske detaljer
Main Authors:	Shek, H, Shek, Howard
Format:	Thesis
Sprog:	English
Udgivet:	1997
Fag:	Smoke plumes Aerodynamics, Hypersonic

Lignende værker

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Experimental methods of hypersonics/
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Hypersonic and high-temperature gas dynamics /
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Computational methods in hypersonic aerodynamics/
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Force measurement techniques in short duration hypersonic facilities
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Boundary layer instabilities in high and low enthalpy hypersonic facilities using high speed schlieren
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Transitional shock wave/boundary-layer interaction unsteadiness on a cone-flare in hypersonic flow
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Design of hypersonic wavecatcher intake at Mach 12 with rectangular-to-elliptical shape transition
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Application of transpiration cooling on hypersonic vehicles to mitigate material oxidation
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Investigation on Infrared Radiation Signatures of Under-Expanded Rocket Exhaust Plumes Due to Angle of Attack
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Udgivet: (2021-01-01)

Experimental results of a Mach 10 conical-flow derived waverider to 14-X hypersonic aerospace vehicle
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Advanced hypersonic test facilities /
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Burning oilwells in Kuwait: smoke plume monitoring and effects on vegetation derived from AVHRR data /
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Boundary layer transition in hypersonic flows
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Development and Application of Computational Tool Using Local Surface Inclination Methods for Preliminary Analysis of Hypersonic Vehicles
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Udgivet: (2020-06-01)

Development and Application of Computational Tool Using Local Surface Inclination Methods for Preliminary Analysis of Hypersonic Vehicles
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Thermal modal analysis of hypersonic composite wing on transient aerodynamic heating
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Aerodynamic Characterization of Hypersonic Transportation Systems and Its Impact on Mission Analysis
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Design and Evaluation of a Hypersonic Waverider Vehicle Using DSMC
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Analysis of aerodynamic characteristics of hypersonic folding-wing aircraft
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Flight-Propulsion Integration Dynamic Analysis and Adaptive Control of the Hypersonic Vehicle at Wide-Range Mach Numbers
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Udgivet: (2022-01-01)

Observed entrainment in a power plant plume
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Udgivet: (2010)

Comprehensive Evaluation of the Massively Parallel Direct Simulation Monte Carlo Kernel “Stochastic Parallel Rarefied-Gas Time-Accurate Analyzer” in Rarefied Hypersonic Flows—Part B: Hypersonic Vehicles
af: Angelos Klothakis, et al.
Udgivet: (2024-10-01)

Trajectory Estimation of Hypersonic Glide Vehicle Based on Analysis of Aerodynamic Performance
Udgivet: (2019-12-01)

Analysis of Aerothermal Environment Characteristics of Hypersonic Rudder Shaft Gaps
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Udgivet: (2025-01-01)

EXPERIMENTAL RESULTS OF A MACH 10 CONICAL-FLOW DERIVED WAVERIDER TO 14-X HYPERSONIC AEROSPACE VEHICLE. doi: 10.5028/jatm.2011.03027510
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Aerodynamics of bodies of revolution/
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COUNTERING HYPERSONIC THREAT
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Udgivet: (2022-10-01)

Aerodynamic Shape Optimization of a Symmetric Airfoil from Subsonic to Hypersonic Flight Regimes
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Udgivet: (2022-11-01)

Variant wing scheme and aerodynamic characteristics analysis of hypersonic vehicle
af: ZHANG Xin, et al.
Udgivet: (2023-08-01)