Experiences performing conceptual design optimization of transport aircraft [PDF]
Optimum Preliminary Design of Transports (OPDOT) is a computer program developed at NASA Langley Research Center for evaluating the impact of new technologies upon transport aircraft.
Arbuckle, P. D., Sliwa, S. M.
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Conceptual design study of a 1985 commercial STOL tilt rotor transport [PDF]
Results of conceptual engineering design studies of a STOL tilt rotor commercial aircraft for the 1985 time frame are presented. The details of aircraft size, performance, flying qualities, noise, and cost are included.
Alexander, H. R. +2 more
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Conceptual Design of a Small Hybrid Unmanned Aircraft System
UAS (Unmanned Aircraft System) technologies are today extremely required in various fields of interest, from military to civil (search and rescue, environmental surveillance and monitoring, and entertainment).
Umberto Papa +2 more
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Conceptual design optimization study [PDF]
The feasibility of applying multilevel functional decomposition and optimization techniques to conceptual design of advanced fighter aircraft was investigated.
Beeman, E. R., II +2 more
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Conceptual design studies of candidate V/STOL lift fan commercial short haul transport for 1980 - 1985 V/STOL lift fan study [PDF]
Conceptual designs of V/STOL lift fan commercial short haul transport aircraft for the 1980-85 time period were studied to determine their technical and economic feasibility. The engine concepts included both integral and remote fans.
Eldridge, W. M. +4 more
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Parametric Aircraft Conceptual Design Space
This paper presents the development of a design framework for the initial conceptual design phase. The focus in this project is on a flexible database in XML format, together with close integration of automated CAD, and other tools, which allows the developed geometry to be used directly in the subsequent preliminary design phase.
Staack, Ingo +7 more
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Conceptual design studies of 1985 commercial VTOL transports that utilized rotors, Volume 2 [PDF]
Results of conceptual design studies of tilt rotor and tandem helicopter aircraft for a 200 nautical mile commercial short haul transport mission are presented.
Alexander, H. R. +2 more
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Structural Analysis in a Conceptual Design Framework [PDF]
Supersonic aircraft designers must shape the outer mold line of the aircraft to improve multiple objectives, such as mission performance, cruise efficiency, and sonic-boom signatures.
Eldred, Lloyd B. +2 more
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Solution Space Analysis for Robust Conceptual Design Solutions in Aeronautics
The use of novel technologies for low-emission and more efficient aviation requires not only the achievement of a given technology readiness level, but also their integration into aircraft concepts.
Vladislav T. Todorov +2 more
doaj +1 more source
Comparison of Structural Concepts for Transport Aircraft with a Tail Cone Turbine [PDF]
An evaluation of three structural concepts for an advanced aircraft design with a tail cone turbine is presented. Structural models were developed using an innovative rapid finite element modeling tool called Conceptual Design Shop (CDS).
Mason, Brian H.
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