Analytical screening of low emissions, high performance duct burners for supersonic cruise aircraft engines [PDF]
An analytical screening study was conducted to identify duct burner concepts capable of providing low emissions and high performance in advanced supersonic engines. Duct burner configurations ranging from current augmenter technology to advanced concepts
Lohmann, R. A., Riecke, G. T.
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Aeronautical Engineering: A special bibliography with indexes, supplement 54 [PDF]
This bibliography lists 316 reports, articles, and other documents introduced into the NASA scientific and technical information system in January ...
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Aeronautical Engineering: A continuing bibliography, supplement 120 [PDF]
This bibliography contains abstracts for 297 reports, articles, and other documents introduced into the NASA scientific and technical information system in February ...
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WIND: Computer program for calculation of three dimensional potential compressible flow about wind turbine rotor blades [PDF]
A computer program is presented which numerically solves an exact, full potential equation (FPE) for three dimensional, steady, inviscid flow through an isolated wind turbine rotor.
Dulikravich, D. S.
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Hyplane: a single-stage suborbital aerospaceplane. [PDF]
CEAS Space J, 2023 Russo G, Voto C.
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Design of transonic compressor cascades using hodograph method [PDF]
The use of the Hodograph Method in the design of a transonic compressor cascade is discussed. The design of the flow mode in the transonic compressor cascade must be as follows: the flow in the nozzle part should be uniform and smooth; the location of ...
Chen, Zuoyi, Guo, Jingrong
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Thermal-Fluid-Solid Coupling-Parametrical Numerical Analysis of Hot Turbine Nozzle Guide Vane. [PDF]
Materials (Basel), 2021 Froissart M, Ochrymiuk T.
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Aeronautical Engineering: A special bibliography with indexes, supplement 51 [PDF]
This bibliography lists 206 reports, articles, and other documents introduced into the NASA Scientific and Technical Information System in November ...
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Numerical study of probe parameters on performance of a transonic axial compressor. [PDF]
PLoS One, 2021 Islam A, Ma H.
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Advanced acoustic and aerodynamic 20-inch fan program [PDF]
The aerodynamic analyses, mechanical analyses, and stress tests of a 20-inch diameter advanced fan design intended for acoustic investigation by NASA-LeRC are discussed.
Erwin, J. R., Heldenbrand, R. W.
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