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Design Studies of the JAPHAR Experimental Vehicle for Dual Mode Ramjet Demonstration

Eggers, T. and Novelli, P. and Haupt, M. (2001) Design Studies of the JAPHAR Experimental Vehicle for Dual Mode Ramjet Demonstration. 10th International Space Planes and Hypersonic Systems and Technologies Conference, Kyoto (ja), 24.-27.04.2001.

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Abstract

Within the DLR - ONERA cooperation JAPHAR (Joint Airbreathing Propulsion for Hypersonic Application Research), the feasibility of a dual mode ramjet engine, combining subsonic and supersonic combustion, is investigated and a methodology for on-ground and inflight performance demonstration is developed. The studies are organised around the blue-print of the experimental vehicle JAPHAR (Fig. 1) which is considered to fly between M = 4 and M = 8. This allows to cover both regimes, subsonic and supersonic combustion. The vehicle provides a solid context and realistic specifications for the different components of the propulsion system. It also answers to one of the fundamental peculiarities of airbreathing propulsion, which is the high level of integration between vehicle and propulsion system requiring a strongly coupled design. This is important not only to establish the propulsive balance but also to obtain a realistic estimation of the component performances. The given paper focusses on the aerodynamic analysis of the main design drivers of the vehicle which are the available thrust, longitudinal trim, longitudinal stability. With view to the application of small leading edge bluntnesses the assessment of the heat loads based on a fluid-structure coupling is presented.

Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=2002, monograph_id=AIAA-Paper: 2001-1921,
Title:Design Studies of the JAPHAR Experimental Vehicle for Dual Mode Ramjet Demonstration
Authors:
AuthorsInstitution or Email of Authors
Eggers, T.UNSPECIFIED
Novelli, P.ONERA
Haupt, M.TU Braunschweig
Date:2001
Status:Published
Keywords:aerodynamic design, hypersonic flow, ramjet, scramjet, flight mechanics, fluid-structure-interaction
Event Title:10th International Space Planes and Hypersonic Systems and Technologies Conference, Kyoto (ja), 24.-27.04.2001
Organizer:AIAA
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Space (old)
HGF - Program Themes:W RP - Raumtransport
DLR - Research area:Space
DLR - Program:W RP - Raumtransport
DLR - Research theme (Project):W - Grundlagen Raumtransport - Anlagen und Messtechnik (old)
Location: Köln-Porz , Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology
Deposited By: Claudia Grant
Deposited On:31 Jan 2006
Last Modified:14 Jan 2010 18:55

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