DETERMINATION OF BURN RATE EQUATION UNCERTAINTY INTERVALS IN SOLID FUEL RAMJET

von Hankins, William J.
Veröffentlicht in AIAA Propulsion and Energy Forum (2021 : Online) Propulsion education (2021)

CHARACTERIZING REACTION DYNAMICS AND DECOMPOSITION PATHWAYS OF NEW SOLID FUELS FOR SCRAMJET AND RAMJET COMBUSTORS

von Berg, Paige
Veröffentlicht in AIAA Propulsion and Energy Forum (2021 : Online) Propulsion education (2021)

AXIAL-INJECTION, END-BURNING HYBRID FUEL GRAIN STUDY

von Hitt, Matthew A.
Veröffentlicht in AIAA Propulsion and Energy Forum (2021 : Online) Hybrid rockets (2021)

DEVELOPMENT OF AN OPTICALLY ACCESSIBLE RACETRACK-TYPE ROTATING DETONATION ROCKET ENGINE

von Unruh, Evan C.
Veröffentlicht in AIAA Propulsion and Energy Forum (2020 : Online) Pressure gain combustion (2020)

DESIGN OF A MOBILE TEST CART FOR LOW-POWER HYBRID MOTORS

von Agnew, Joseph F.
Veröffentlicht in AIAA Propulsion and Energy Forum (2020 : Online) Propulsion education (2020)

EXPERIMENTAL STUDY OF A RACETRACK-TYPE ROTATING DETONATION ROCKET ENGINE WITH SHEAR-COAXIAL INJECTORS RUN ON GASEOUS METHANE AND OXYGEN

von Unruh, Evan C.
Veröffentlicht in AIAA Propulsion and Energy Forum (2021 : Online) Pressure gain combustion (2021)

UNCERTAINTY ANALYSIS OF EXPERIMENTAL DISCHARGE COEFFICIENTS IN ADDITIVELY MANUFACTURED LIQUID INJECTOR ELEMENTS

von Venters, James P.
Veröffentlicht in AIAA Propulsion and Energy Forum (2019 : Indianapolis, Ind.) Liquid propulsion ; Volume 1 of 2 (2019)

Mixing and Recovery Performance of Triplet Impinging Injectors with Varying Flow Areas for Detonative Combustion

von Hemming, Michaela R.
Veröffentlicht in AIAA SciTech Forum (2023 : National Harbor, Md.; Online) Pressure gain combustion (2023)