Numerical simulation of the hypersonic flow around lifting vehicles [PDF]
A method for solving the viscous hypersonic flow field around realistic configurations is presented. The numerical procedure for generating the required finite difference grid and the two-factored implicit flow solver are described. Results are presented
Chaussee, Denny +2 more
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Prediction of forces and moments for flight vehicle control effectors. Part 1: Validation of methods for predicting hypersonic vehicle controls forces and moments [PDF]
Many types of hypersonic aircraft configurations are currently being studied for feasibility of future development. Since the control of the hypersonic configurations throughout the speed range has a major impact on acceptable designs, it must be ...
Maughmer, Mark D. +3 more
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Prediction of forces and moments for hypersonic flight vehicle control effectors [PDF]
This research project includes three distinct phases. For completeness, all three phases of the work are briefly described in this report. The goal was to develop methods of predicting flight control forces and moments for hypersonic vehicles which could
Guilmette, Neal +3 more
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Efficient adaptive constrained control with time-varying predefined performance for a hypersonic flight vehicle [PDF]
, 2017 Caisheng Wei +4 more
openalex +1 more source
Comparative study of turbulence models in predicting hypersonic inlet flows [PDF]
A numerical study was conducted to analyze the performance of different turbulence models when applied to the hypersonic NASA P8 inlet. Computational results from the PARC2D code, which solves the full two-dimensional Reynolds-averaged Navier-Stokes ...
Anderson, Bernhard H. +2 more
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An investigation of starting processes and flow patterns occurring in hypersonic axisymmetric inlets of internal compression [PDF]
, 2017 Yu. P. Gounko, I. I. Mazhul, N. I. Kavun
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Investigation of nose bluntness and angle of attack effects on slender bodies in viscous hypersonic flows [PDF]
Hypersonic flows over cones and straight biconic configurations are calculated for a wide range of free stream conditions in which the gas behind the shock is treated as perfect.
Sehgal, A. K. +2 more
core +1 more source
Iterative Learning Control Combination with Adaptive Sliding Mode Technique for a Hypersonic Vehicle [PDF]
, 2019 Xiaodong Lu +3 more
openalex +1 more source