Some forms of the one-dimensional wave-equation for inviscid flows

Aerospace Engineerin

Derivation of the solid propellant responce function

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The double Helmholtz resonator as a possible tool for the determination of the responce function of solid rocket propellants in the low frequency range

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An estimate of heat transfer in L* burners

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The determination of temperature histories in a cylindrical ring, heated by convection

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Verslag van een studiereis naar California van 12 t/m 26 januari 1980

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A one-dimensional analysis of acoustic pressure fluctuations in a simple rocket motor

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Experimental investigation of the Helmholtz resonator burner; Three months at China lake

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Verslag van bezoeken van IMI-Summerfield, Kidderminster, PERME, Westcott

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The determination of the throat conditions for equilibrium and frozen flows in rocket motor nozzles

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