C
C Engelund Walter
Researcher at Langley Research Center
Publications - 5
Citations - 152
C Engelund Walter is an academic researcher from Langley Research Center. The author has contributed to research in topics: Propulsion & Aerodynamics. The author has an hindex of 5, co-authored 5 publications receiving 151 citations.
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Proceedings ArticleDOI
Aerodynamic Database Development for the Hyper-X Airframe Integrated Scramjet Propulsion Experiments
TL;DR: In this paper, the authors provide an overview of the activities associated with the development of the Hyper-X aerodynamic database, including wind tunnel test activities and parallel CFD analysis efforts for all phases of the hyper-X flight tests.
Proceedings ArticleDOI
Prediction and Validation of Mars Pathfinder Hypersonic Aerodynamic Data Base
A Gnoffo Peter,D Braun Robert,Weilmuenster K. James,A Mitcheltree Robert,C Engelund Walter,W Powell Richard +5 more
TL;DR: In this article, post-flight analysis of the Mars Pathfinder hypersonic, continuum aerodynamic data base is presented, which includes accelerations along the body axis and axis normal directions.
Proceedings ArticleDOI
Six Degree-of-Freedom Entry Dispersion Analysis for the METEOR Recovery Module
TL;DR: In this article, the authors performed a six degree-of-freedom entry dispersion analysis for the Multiple Experiment Transporter to Earth Orbit and Return (METEOR) mission to quantify the impact of various exo-atmospheric and atmospheric uncertainties.
Propulsion System Airframe Integration Issues and Aerodynamic Database Development for the Hyper-X Flight Research Vehicle
TL;DR: In this article, the authors provide an overview of the current activities associated with the development of the Hyper-X aerodynamic database, including wind tunnel test activities and parallel CFD analysis efforts.
Proceedings ArticleDOI
Integrated Aero-Propulsive CFD Methodology for the Hyper-X Flight Experiment
Jr Charles E. Cockrell,C Engelund Walter,D Bittner Robert,D Dilley Arthur,N Jentink Tom,Frendi Abdelkader +5 more
TL;DR: In this paper, the authors describe analysis tools used and the methodology for obtaining pre-flight predictions of longitudinal performance increments for the X-43 Hyper-X Research Vehicle (HXRV).