The ''delta p'' approach from Nike combustion instability

Hisler, A.

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NASA NTRS · 19660026016

The ''delta p'' approach from Nike combustion instability

Hisler, A.

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Abstract

Applicability of delta p approach to study of combustion instability in liquid and solid propellant rocket engines

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STAGNATION FLOW SOLID PROPELLANT ROCKET ENGINE LIQUID PROPELLANT ROCKET ENGINE COMBUSTION INSTABILITY

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Hisler, A.. 1965-10-04. The ''delta p'' approach from Nike combustion instability. https://ntrs.nasa.gov/citations/19660026016

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