[go: up one dir, main page]

Johnson et al., 2009 - Google Patents

Rotorcraft conceptual design environment

Johnson et al., 2009

View PDF
Document ID
4019966421214538433
Author
Johnson W
Sinsay J
Publication year

External Links

Snippet

Requirements for a rotorcraft conceptual design environment are discussed, from the perspective of a government laboratory. Rotorcraft design work in a government laboratory must support research, by producing technology impact assessments and defining the …
Continue reading at apps.dtic.mil (PDF) (other versions)

Classifications

    • G—PHYSICS
    • G06—COMPUTING; CALCULATING; COUNTING
    • G06F—ELECTRICAL DIGITAL DATA PROCESSING
    • G06F17/00—Digital computing or data processing equipment or methods, specially adapted for specific functions
    • G06F17/50—Computer-aided design
    • G06F17/5009—Computer-aided design using simulation
    • G06F17/5018—Computer-aided design using simulation using finite difference methods or finite element methods
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies
    • Y02T50/67—Relevant aircraft propulsion technologies
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Similar Documents

Publication Publication Date Title
Botero et al. Suave: An open-source environment for conceptual vehicle design and optimization
Keane et al. Computational approaches for aerospace design: the pursuit of excellence
Brelje et al. Development of a conceptual design model for aircraft electric propulsion with efficient gradients
Lukaczyk et al. SUAVE: an open-source environment for multi-fidelity conceptual vehicle design
Schmollgruber et al. Use of a certification constraints module for aircraft design activities
Liersch et al. Conceptual design and aerodynamic analyses of a generic UCAV configuration
Chakraborty et al. Generalized energy-based flight vehicle sizing and performance analysis methodology
Moerland et al. On the design of a strut-braced wing configuration in a collaborative design environment
Mistree et al. The design of aircraft using the decision support problem technique
Schültke et al. MICADO: overview of recent developments within the conceptual aircraft design and optimization environment
Goertz et al. Overview of collaborative multi-fidelity multidisciplinary design optimization activities in the DLR project VicToria
MacDonald et al. SUAVE: An open-source environment enabling unconventional vehicle designs through higher fidelity
Liersch et al. Multidisciplinary design and aerodynamic assessment of an agile and highly swept aircraft configuration
Sitaraman et al. Rotor loads prediction using helios: a multisolver framework for rotorcraft aeromechanics analysis
Perullo et al. Effects of advanced engine technology on open rotor cycle selection and performance
Wissink et al. Overview of new capabilities in helios version 9.0
Misiorowski et al. Computational analysis of rotor-blown-wing for electric rotorcraft applications
Morris et al. Mob-a european project on multidisciplinary design optimisation
Sheng et al. Computational simulation and analysis of bell boeing quad tiltrotor aero interaction
Ruh et al. Large-scale multidisciplinary design optimization of the NASA lift-plus-cruise concept using a novel aircraft design framework
Johnson et al. Rotorcraft conceptual design environment
Ciampa et al. Preliminary design for flexible aircraft in a collaborative environment
Piperni et al. The application of multi-disciplinary optimization technologies to the design of a business jet
Khalid Development and implementation of rotorcraft preliminary design methodology using multidisciplinary design optimization
Thai Development of high-fidelity computational methods for prediction of multirotor aerodynamics, aeroacoustics, and trim