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Aerodynamic Design of a Waverider Configuration Adapted to "Once-Around-Earth"-Requirements

Eggers, Th. (1997) Aerodynamic Design of a Waverider Configuration Adapted to "Once-Around-Earth"-Requirements. DLR-Interner Bericht. 129-97/15, 40 S.

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Abstract

The present report summarizes the DLR contribution to the FESTIP/I - Slice B system study (WP 4015b). The objective of the study was the aerodynamic design of a waverider configuration adapted to "Once-Around-Earth" requirements (concept FSS-15WR). This includes the definition of a surface geometry, an aerodynamic dataset for the whole flow regime an the estimation of heat loads for selected trajectory points. Based on the aerodynamic coefficients a first complete aerodynamic dataset and a first reference trajectory for a waverider based configurations was established. The report closes with some recommendations for a second design cycle and points out potential weak points of the designed waverider based shape FSS-15WR.

Document Type:Monograph (DLR-Interner Bericht)
Additional Information: LIDO-Berichtsjahr=1997,
Title:Aerodynamic Design of a Waverider Configuration Adapted to "Once-Around-Earth"-Requirements
Authors:
AuthorsInstitution or Email of Authors
Eggers, Th.UNSPECIFIED
Date:1997
Number of Pages:40
Status:Published
Keywords:Design of hypersonic cruise vehicles, hypersonic waveriders
HGF - Research field:UNSPECIFIED
HGF - Program:Space (old)
HGF - Program Themes:W RP - Raumtransport
DLR - Research area:UNSPECIFIED
DLR - Program:W RP - Raumtransport
DLR - Research theme (Project):W - Zukünftige Raumtransporter - Entwurf und Simulationsmethoden für Raumtransporter (old)
Location: Köln-Porz , Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Institut für Entwurfsaerodynamik
Deposited By: elib DLR-Beauftragter
Deposited On:03 Apr 2006
Last Modified:27 Apr 2009 10:06

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