A modified method of integral relations approach to the blunt-body equilibrium air flow field, including comparisons with inverse solutions [PDF]
Numerical calculation of inviscid adiabatic flow field around blunt bodies at hypersonic ...
Garrett, L. B. +2 more
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A Survey of Hypersonic-Ramjet Concepts [PDF]
, 1959 A brief discussion is presented of the major problem areas involved in the development of a hypersonic ramjet engine. Keeping the structural temperature to an acceptably low level is the severest problem expected.
Weber, R. J.
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RBFNN-Based Anti-Input Saturation Control for Hypersonic Vehicles
AerospaceIn hypersonic flight control, characterized by challenges posed by input saturation, model parameter uncertainties, and external disturbances, this paper introduces a pioneering anti-input saturation control method based on RBFNN adaptivity.
Bangchu Zhang +4 more
doaj +1 more source
Free-flight measurements of stagnation-point convective heat transfer at velocities to 41,000 ft/sec [PDF]
Free flight measurements of stagnation point convective heat transfer in air at hypersonic ...
Compton, D. L., Cooper, D. M.
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X-15, Research at the Edge of Space [PDF]
, 1963 X-15 project - history, aircraft design, operational systems, & flight ...
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Shock-Wave Effects on the Laminar Skin Friction of an Insulated Flat Plate at Hypersonic Speeds [PDF]
, 1953 Ting-Yi Li, H. T. Nagamatsu
openalex +1 more source
NUMERICAL MODELING AND DYNAMIC SIMULATIONS OF NONLINEAR AEROTHERMOELASTIC OF A DOUBLE-WEDGE LIFTING SURFACE [PDF]
Journal of Engineering Science and Technology, 2008 The design of the re-entry space vehicles and high-speed aircrafts requires special attention to the nonlinear thermoelastic and aerodynamic instabilities of their structural components.
ARIF A. EBRAHEEM AL-QASSAR
doaj
Modeling and control of hypersonic vehicle dynamic under centroid shift
Advances in Mechanical Engineering, 2018 Due to the huge flight scale and the fast speed of hypersonic vehicle, the system must be of strong nonlinearity, coupling, and fast time variability, which give rise to the huge challenge for the design of controller.
Yizhen Meng, Bin Jiang, Ruiyun Qi
doaj +1 more source
arXiv, 2009 A method and facilities for delivering payload and people into outer space are presented. This method uses, in general, engines located on a planetary surface. The installation consists of a space apparatus, power drive stations, which include a flywheel accumulator (for storage) of energy, a variable reducer, a powerful homopolar electric generator ...
arxiv
Structural concepts and experimental considerations for a versatile high-speed research airplane [PDF]
Future aircraft may be hydrogen fueled and fly at hypersonic speeds. The resulting environments will require new structural concepts to satisfy performance goals.
Jackson, L. R. +2 more
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