Disputatio medica inauguralis De asthmate

von Baird, George Husband
Veröffentlicht 1827

AN ASSESSMENT ON THE UNSTEADY FLOW DISTORTION GENERATED BY AN S-DUCT INTAKE

von Migliorini, Matteo
Veröffentlicht in AIAA Propulsion and Energy Forum (2019 : Indianapolis, Ind.) Inlets, nozzles, and propulsion systems integration (2019)

IMPACT OF DROOP AND SCARF ON THE AERODYNAMIC PERFORMANCE OF COMACT AERO-ENGINE NACELLES

von Tejero, Fernando
Veröffentlicht in AIAA SciTech Forum and Exposition (2020 : Orlando, Fla.) Applied aerodynamics ; Volume 3 of 4 (2020)

THE IMPACT OF INLET BOUNDARY LAYER THICKNESS ON THE UNSTEADY AERODYNAMICS OF S-DUCT INTAKES

von Migliorini, Matteo
Veröffentlicht in AIAA Propulsion and Energy Forum (2019 : Indianapolis, Ind.) Inlets, nozzles, and propulsion systems integration (2019)

Characterization of Unsteady Distortion Events for S-Duct Intakes Under Non-Uniform Inlet Conditions

von Migliorini, Matteo
Veröffentlicht in AIAA SciTech Forum (2023 : National Harbor, Md.; Online) Inlets, nozzles, and propulsion systems integration (2023)

Computational Assessment of Non-Axisymmetric Separate-Jet Exhausts on Test Rig Configurations

von Hueso-Rebassa, Josep
Veröffentlicht in AIAA Aviation Forum (2023 : San Diego, Calif.; Online) Inlets, nozzles, and propulsion systems integration (2023)

GEOMETRY PARAMETERISATION AND AERODYNAMIC CHARACTERISTICS OF AXISYMMETRIC AFTERBODIES

von Zuccolo, Giovanni
Veröffentlicht in AIAA SciTech Forum and Exposition (2020 : Orlando, Fla.) Applied aerodynamics ; Volume 4 of 4 (2020)

EFFECTS OF AIRCRAFT INTEGRATION ON COMPACT NACELLE AERODYNAMICS

von Tejero, Fernando
Veröffentlicht in AIAA SciTech Forum and Exposition (2020 : Orlando, Fla.) Applied aerodynamics ; Volume 4 of 4 (2020)

Computational Assessment of Non-Axisymmetric Separate-Jet Exhausts on Test Rig Configurations

von Hueso-Rebassa, Josep
Veröffentlicht in AIAA Aviation Forum (2023 : San Diego, Calif.; Online) Applied aerodynamics ; Volume 1 of 5 (2023)

LOW ORDER MODELS FOR TRANSONIC AFTERBODY AERODYNAMIC CHARACTERISTICS

von Zuccolo, Giovanni
Veröffentlicht in AIAA SciTech Forum and Exposition (2020 : Orlando, Fla.) Applied aerodynamics ; Volume 4 of 4 (2020)

Design Considerations of Non-Axisymmetric Exhausts for Large Civil Aero-Engines

von Hueso-Rebassa, Josep
Veröffentlicht in AIAA Aviation Forum (2023 : San Diego, Calif.; Online) Inlets, nozzles, and propulsion systems integration (2023)

Understanding Heisenberg's "magical" paper of July 1925 : a new look at the calculational details

von Aitchison, Ian Johnston Rhind
Veröffentlicht in American journal of physics / publ. by the American Institute of Physics (2004)

UNSTEADY SWIRL DISTORTION CHARACTERISTICS FOR S-DUCTS USING LATTICE BOLTZMANN, TIME-RESOLVED, STEREO PIV METHODS

von Guerrero-Hurtado, Manuel
Veröffentlicht in AIAA Propulsion and Energy Forum (2019 : Indianapolis, Ind.) Inlets, nozzles, and propulsion systems integration (2019)

GT2021-60029 The Use of Enhanced Nozzlie Maps for Gas-Turbine Performance Modelling

von Al-Akam, Aws A.
Veröffentlicht in ASME Turbo Expo (2021 : Online) Proceedings of ASME Turbo Expo 2021: Turbomachinery Technical Conference and Exposition ; Volume 1: Aircraft engine, fans and blowers, marine, wind energy, scholar lecture (2021)

Design and Optimisation of a Mach 2.5 Wind Tunnel Nozzle

von Moreno, Miguel
Veröffentlicht in AIAA SciTech Forum (2023 : National Harbor, Md.; Online) Inlets, nozzles, and propulsion systems integration (2023)

Experimental Investigation of External Fan Cowl Separation for Compact Nacelles in Windmilling Scenarios

von Sabnis, Kshitij
Veröffentlicht in AIAA Aviation Forum (2023 : San Diego, Calif.; Online) Applied aerodynamics ; Volume 1 of 5 (2023)

GT2020-14470 Robust Aerodynamic Design of Nacelles for Future Civil Aero-Engines

von Schreiner, B. Deneys J.
Veröffentlicht in ASME Turbo Expo (2020 : Online) Proceedings of the ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition - 2020 ; Volume 1: Aircraft engine - fans and blowers (2020)

Design of a High-Speed Intake Distortion Simulator for Propulsion Integration Research

von Migliorini, Matteo
Veröffentlicht in AIAA SciTech Forum (2023 : National Harbor, Md.; Online) Inlets, nozzles, and propulsion systems integration (2023)

Deep-Learning Methods for Non-Linear Transonic Flow-Field Prediction

von Sureshbabu, Sanjeeth
Veröffentlicht in AIAA Aviation Forum (2023 : San Diego, Calif.; Online) Multidisciplinary design optimization ; Volume 1 of 2 (2023)

Characteristics of Shock-Induced Boundary Layer Separation on Nacelles Under Windmilling Diversion Conditions

von Boscagli, Luca
Veröffentlicht in AIAA Aviation Forum (2023 : San Diego, Calif.; Online) Applied aerodynamics ; Volume 1 of 5 (2023)