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Aerospace engineering. arama terimini sil

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SpringerLink (Online service)

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Baqersad, Javad. editor.

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Barakos, George N. editor.

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California State University, Long Beach. Mechanical and Aerospace Engineering. degree granting institution.

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Castillo, Luciano. editor.

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Chen, Alexander J., author.

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Chhunchha, Aakash C., author.

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Cranfield University (United Kingdom). College of Aeronautics. degree granting institution.

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Cranfield University (United Kingdom). School of Engineering, Optical Sensors Group. degree granting institution.

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Danaila, Luminita. editor.

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Dodoo-Amoo, David Nii Darku, author.

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Doerffer, Piotr. editor.

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Electronic Navigation Research Institute. editor.

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Ganesan, Vishwanath, author.

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Glauser, Mark. editor.

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Greenfield, Harvey, author.

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Harvie, Julie M. editor.

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Luczak, Marcin M. editor.

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North Carolina Agricultural and Technical State University. Mechanical Engineering. degree granting institution.

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Odic, Richard Marie, author.

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Old Dominion University. Mechanical & Aerospace Engineering. degree granting institution.

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Pasaribu, H. M., author.

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Pollard, Andrew. editor.

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Purdue University. Mechanical Engineering. degree granting institution.

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Rothwell, Alan. author.

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Salvetti, Maria Vittoria. editor.

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Sheng, Chunhua. author.

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University of Glasgow (United Kingdom). Department of Aeronautics and Fluid Mechanics. degree granting institution.

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d'Agostino, Luca. editor.

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Advances in Transitional Flow Modeling Applications to Helicopter Rotors için kapak resmi

Advances in Transitional Flow Modeling Applications to Helicopter Rotors

1.

Advances in Transitional Flow Modeling Applications to Helicopter Rotors

by

Sheng, Chunhua. author.

http://dx.doi.org/10.1007/978-3-319-32576-7

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Alıntı:

aerodynamic design and the analysis of fixed-wing or rotary wing aircraft, while also offering advanced

Aerodynamic Heating Analysis of Re-entry Space Capsule Using Computational Fluid Dynamics için kapak resmi

Aerodynamic Heating Analysis of Re-entry Space Capsule Using Computational Fluid Dynamics

2.

Aerodynamic Heating Analysis of Re-entry Space Capsule Using Computational Fluid Dynamics

by

Chhunchha, Aakash C., author.

http://gateway.proquest.com/openurl?url_ver=Z39.88-2004&rft_val_fmt=info:ofi/fmt:kev:mtx:dissertation&res_dat=xri:pqm&rft_dat=xri:pqdiss:10752510

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obtained by means of benchmark empirical formulation is compared to the CFD analysis. An additional

Optimization Methods in Structural Design için kapak resmi

Optimization Methods in Structural Design

3.

Optimization Methods in Structural Design

by

Rothwell, Alan. author.

http://dx.doi.org/10.1007/978-3-319-55197-5

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Alıntı:

Problem -- 4 Numerical Methods for Unconstrained Optimization -- 5 Numerical Methods for Constrained

Air Traffic Management and Systems II Selected Papers of the 4th ENRI International Workshop, 2015 için kapak resmi

Air Traffic Management and Systems II Selected Papers of the 4th ENRI International Workshop, 2015

4.

Air Traffic Management and Systems II Selected Papers of the 4th ENRI International Workshop, 2015

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Electronic Navigation Research Institute. editor.

http://dx.doi.org/10.1007/978-4-431-56423-2

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-- Quantitative Analysis of Conflict between Aircraft by Using Radar Track Data -- Optimizing the Design of a

Non-uniformities in shock tube flow with emphasis on reflected shock curvature için kapak resmi

Non-uniformities in shock tube flow with emphasis on reflected shock curvature

5.

Non-uniformities in shock tube flow with emphasis on reflected shock curvature

by

Greenfield, Harvey, author.

http://gateway.proquest.com/openurl?url_ver=Z39.88-2004&rft_val_fmt=info:ofi/fmt:kev:mtx:dissertation&res_dat=xri:pqm&rft_dat=xri:pqdiss:10867806

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series analysis is formed with subsequent addition of numerical analysis by computer utilisation. The

Volterra Series Approximation for Multi-Degree of Freedom, Multi-Input, Multi-Output, Aircraft Dynamics için kapak resmi

Volterra Series Approximation for Multi-Degree of Freedom, Multi-Input, Multi-Output, Aircraft Dynamics

6.

Volterra Series Approximation for Multi-Degree of Freedom, Multi-Input, Multi-Output, Aircraft Dynamics

by

Chen, Alexander J., author.

http://gateway.proquest.com/openurl?url_ver=Z39.88-2004&rft_val_fmt=info:ofi/fmt:kev:mtx:dissertation&res_dat=xri:pqm&rft_dat=xri:pqdiss:10813977

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effective analysis to the cause and effect of the response. Individual responses of each nonlinear component

Cavitation Instabilities and Rotordynamic Effects in Turbopumps and Hydroturbines Turbopump and Inducer Cavitation, Experiments and Design için kapak resmi

Cavitation Instabilities and Rotordynamic Effects in Turbopumps and Hydroturbines Turbopump and Inducer Cavitation, Experiments and Design

7.

Cavitation Instabilities and Rotordynamic Effects in Turbopumps and Hydroturbines Turbopump and Inducer Cavitation, Experiments and Design

by

d'Agostino, Luca. editor.

http://dx.doi.org/10.1007/978-3-319-49719-8

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, visualization and analysis of cavitating flows, and introduces the main aspects of the hydrodynamic design and

Raman optical time domain reflectometry for aircraft fire-overheat detection and monitoring için kapak resmi

Raman optical time domain reflectometry for aircraft fire-overheat detection and monitoring

8.

Raman optical time domain reflectometry for aircraft fire-overheat detection and monitoring

by

Odic, Richard Marie, author.

http://gateway.proquest.com/openurl?url_ver=Z39.88-2004&rft_val_fmt=info:ofi/fmt:kev:mtx:dissertation&res_dat=xri:pqm&rft_dat=xri:pqdiss:10832209

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-Diodes (APD) and by the cascaded amplification modules, the numerical signals were processed using digital

An approach to configuration design synthesis of subsonic transport aircraft using artificial intelligence techniques için kapak resmi

An approach to configuration design synthesis of subsonic transport aircraft using artificial intelligence techniques

9.

An approach to configuration design synthesis of subsonic transport aircraft using artificial intelligence techniques

by

Pasaribu, H. M., author.

http://gateway.proquest.com/openurl?url_ver=Z39.88-2004&rft_val_fmt=info:ofi/fmt:kev:mtx:dissertation&res_dat=xri:pqm&rft_dat=xri:pqdiss:10832381

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Alıntı:

reasoning process of the aircraft configuration definition and the numerical analyses that lie behind the

An Error Analysis of the Integral Differential Scheme Navier-Stokes Solver için kapak resmi

An Error Analysis of the Integral Differential Scheme Navier-Stokes Solver

10.

An Error Analysis of the Integral Differential Scheme Navier-Stokes Solver

by

Dodoo-Amoo, David Nii Darku, author.

http://gateway.proquest.com/openurl?url_ver=Z39.88-2004&rft_val_fmt=info:ofi/fmt:kev:mtx:dissertation&res_dat=xri:pqm&rft_dat=xri:pqdiss:10786260

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' solutions in comparison to the numerical solutions generated by a wide range of numerical solutions at

Development of a Finite Volume General Two-Phase Navier-Stokes Solver for Direct Numerical Simulations on Cut-Cells with Sharp Fixed Interface için kapak resmi

Development of a Finite Volume General Two-Phase Navier-Stokes Solver for Direct Numerical Simulations on Cut-Cells with Sharp Fixed Interface

11.

Development of a Finite Volume General Two-Phase Navier-Stokes Solver for Direct Numerical Simulations on Cut-Cells with Sharp Fixed Interface

by

Ganesan, Vishwanath, author.

http://gateway.proquest.com/openurl?url_ver=Z39.88-2004&rft_val_fmt=info:ofi/fmt:kev:mtx:dissertation&res_dat=xri:pqm&rft_dat=xri:pqdiss:10808593

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Taylor-Green vortex field and a detailed Von-Neumann stability analysis is performed for solving a linear

Recent Progress in Flow Control for Practical Flows Results of the STADYWICO and IMESCON Projects için kapak resmi

Recent Progress in Flow Control for Practical Flows Results of the STADYWICO and IMESCON Projects

12.

Recent Progress in Flow Control for Practical Flows Results of the STADYWICO and IMESCON Projects

by

Doerffer, Piotr. editor.

http://dx.doi.org/10.1007/978-3-319-50568-8

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-Structure Interaction Simulation -- Analysis and Optimization of Flow Around Flexible Wings and Blades Using the

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