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Low pressure gas flow analysis through an effusive inlet using mass spectrometry final report, period ending 31 Dec, 1987 / by Brown, David Robert, 1963-

Quasi non-intrusive sampling and analysis of gases associated with the boundary layer on the tethered satellite and similar supersonic and hypersonic research vehicles by Brown, Kenneth G.

Shock-tunnel combustor testing for hypersonic vehicles by Loomis, Mark

Lessons learned during TBCC design for the NASA-AFRL joint system study / by Snyder, Christopher A., Espinosa E., José M.

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A zonal computational procedure adapted to the optimization of two-dimensional thrust augmentor inlets by Lund, Thomas S.

Asymptotic high frequency analysis of the electromagnetic backscattering from an inlet model consisting of piecewise linearly tapered sections by Altintas, A.

PTA testbed aircraft engine inlet model test report

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TFaNS T⁺łone F̲a̲n N⁺łoise Design/Prediction S̲ystem by Topol, David A.

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Internal thrust and pumping performance of an auxiliary inlet ejector nozzle with clamshell thrust reverser / by Mansour, Ali H. (Ali Hafiz), Burley, Richard R.

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