Results 21 to 30 of about 139,373 (174)
Effects of Sidewall Compression and Relaminarization in a Scramjet Inlet [PDF]
, 2013 This paper presents the numerical simulations and the performance analysis of a scramjet inlet as part of a combined experimental and numerical study.
Hohn, Oliver +4 more
core +1 more source
International Journal of Aerospace Engineering, Volume 2022, Issue 1, 2022., 2022 Liquid oxygen chill‐down in a vertical exit‐contracted pipe was investigated experimentally. The wall temperatures were recorded in detail to describe the filling and chill‐down process of the experimental section. Two quenching fronts, the exit one and the inlet one, were detected, and their propagations were found.
Jiaqi Zhang +3 more
wiley +1 more source
Numerical Investigations of the Effects of Sidewall Compression and Relaminarization in 3D Scramjet Inlet [PDF]
, 2011 This paper presents the numerical simulations and performance analysis of a 3D scramjet inlet with focus on the effects of sidewall compression and relaminarization. A well-validated finite volume flow solver was used to simulate a scramjet inlet with a
Marek Behr +9 more
core +1 more source
Lagrange Optimization of Shock Waves for Two-Dimensional Hypersonic Inlet with Geometric Constraints
Aerospace, 2022 The present paper focuses on the Lagrange optimization of shock waves for a two-dimensional hypersonic inlet by limiting the cowl internal angle and inlet length.
Yuling Li +4 more
doaj +1 more source
Numerical Study on Pipeline Pressure Surge of the Large Aircraft Fuel System
Shock and Vibration, Volume 2022, Issue 1, 2022., 2022 The sudden closure of the refueling valve during the refueling process will cause the water hammer phenomenon in the pipeline of the large aircraft fuel system and produce pressure waves propagating along the pipeline. In serious cases, it will cause severe damage to the pipeline.
Yi Tu +5 more
wiley +1 more source
Analysis of a Three-Dimensional, High Pressure Ratio Scramjet Inlet with Variable Internal Contraction [PDF]
, 2012 We conducted an extensive experimental examination of the operational behavior of a three-dimensional scramjet inlet featuring a movable cowl to adapt the internal contraction according to the respective operation conditions.
Hohn, Oliver +3 more
core +1 more source
International Journal of Chemical Engineering, Volume 2022, Issue 1, 2022., 2022 The technology of flame stabilization on cavity‐based scramjet combustor has great significance in the field of future spacecraft. In this paper, a compressible modified FGM model was established based on the idea of the flamelet model, which was adopted to simulate the unsteady combustion process of the hydrogen transverse jet in the upper cavity of ...
Qi Zhang +4 more
wiley +1 more source
Experimental Investigation on the Influence of Sidewall Compression on the Flowfield of a Scramjet Inlet at Mach 7 [PDF]
, 2011 In this paper, we present the results of an extensive measurement campaign to investigate the effect of external and internal sidewall compression as well as different contraction ratios on the performance of the flowfield of a scramjet inlet ...
Ali Gülhan +3 more
core +1 more source
Experimental Investigation on the Influence of Yaw Angle on the Inlet Performance at Mach 7 [PDF]
, 2010 This paper presents the results of an extensive measurement campaign that was conducted with an two-dimensional hypersonic inlet in the Hypersonic Windtunnel H2K at the German Aerospace Center in Cologne in order to study the effects of angle of yaw on ...
Ali Gülhan +3 more
core +1 more source
Study on Three-Dimensional Inner Flow Field Characteristics and Performance of Scramjet [PDF]
MATEC Web of Conferences, 2019 The three-dimensional characteristics and performance of the flow field in the inlet of the scramjet engine were numerically simulated by CFD software. The flow characteristics in the width direction of the inlet and the influence of the aspect ratio on ...
Gao Feng, Zhao Jie, Zhang Cheng Tao
doaj +1 more source