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CISAP: Cruise Speed Impact on Supersonic Aircraft Planform; a Project Overview

Herrmann, U. (2004) CISAP: Cruise Speed Impact on Supersonic Aircraft Planform; a Project Overview. 10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, Albany/New York (usa), 30.08.-01.09.2004.

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Abstract

Defining and executing the EREA - Airbus project called "CISAP", reflects continued interest of European industry in supersonic flight technology. CISAP reads "Cruise speed impact on Supersonic Aircraft planform" and the project addresses mainly two topics: first the development, set-up and verification of several mixed fidelity multiple-discipline optimization (MDO) processes and secondly the application of these processes to optimize wing planforms of Supersonic Commercial Transports (SCT) for maximum range at different supersonic cruise Mach-numbers. This is how the impact of the cruise Mach number on the aircraft planform and the overall aircraft performance is demonstrated. Datum configurations to start the MDO design work from are defined using conceptual design methods for two lower cruise Mach numbers. The configurations transporting 250 passengers are designed for a target range of 5500 nautical miles and a fixed maximum take-off weight. Applying different MDO methods within CISAP to maximize the range of the datum configurations leads to significant planform changes of all aircraft. The computed multiple discipline performance increases show large benefits for aircraft flying at lower supersonic Mach numbers. The experience gained while applying these processes indicates further optimization potential of the designed configurations as well as modelling improvements of the developed MDO processes.

Item URL in elib:https://elib.dlr.de/12997/
Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=2005, monograph_id=AIAA-paper 2004-4539,
Title:CISAP: Cruise Speed Impact on Supersonic Aircraft Planform; a Project Overview
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Herrmann, U.UNSPECIFIEDUNSPECIFIED
Date:2004
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Multidisciplinary, Planform design, high-fidelity codes, cruise range increases
Event Title:10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, Albany/New York (usa), 30.08.-01.09.2004
Organizer:AIAA
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research (old)
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Concepts & Integration (old)
Location: Köln-Porz , Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology
Deposited By: Grant, Claudia
Deposited On:31 Jan 2006
Last Modified:14 Jan 2010 19:48

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