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Development of a TRL 3 Concept for Variable Pitot Inlets for SST

Kazula, Stefan and Höschler, Klaus (2022) Development of a TRL 3 Concept for Variable Pitot Inlets for SST. ISABE 2022, 2022-09-25 - 2022-09-30, Ottawa, Kanada.

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Abstract

An overview of aero-engine inlets, the design process in aviation and a safe design approach for academic studies is provided. By means of a safe design approach, a variable inlet concept is developed up to technology readiness level (TRL) 3 and described. The application of safety and reliability methods, aerodynamic and structural analyses, as well as functional demonstrators proves the feasibility of the present variable inlet concept and highlights its potential for application in future supersonic transport (SST).

Item URL in elib:https://elib.dlr.de/189943/
Document Type:Conference or Workshop Item (Speech)
Title:Development of a TRL 3 Concept for Variable Pitot Inlets for SST
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Kazula, StefanUNSPECIFIEDhttps://orcid.org/0000-0002-9050-1292UNSPECIFIED
Höschler, KlausBTU Cottbus-SenftenbergUNSPECIFIEDUNSPECIFIED
Date:October 2022
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Variable Pitot Inlet; Supersonic Transport; Concept Development
Event Title:ISABE 2022
Event Location:Ottawa, Kanada
Event Type:international Conference
Event Start Date:25 September 2022
Event End Date:30 September 2022
Organizer:International Society for Air Breathing Engines
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Clean Propulsion
DLR - Research area:Aeronautics
DLR - Program:L CP - Clean Propulsion
DLR - Research theme (Project):L - Future Engines and Engine Integration
Location: Cottbus
Institutes and Institutions:Institute of Electrified Aero Engines
Deposited By: Kazula, Stefan
Deposited On:17 Nov 2022 10:10
Last Modified:24 Apr 2024 20:51

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