Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 84
Book Description
Calculation of Unsteady Aerodynamics for Four AGARD Standard Aeroelastic Configurations
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 84
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 84
Book Description
Unsteady Transonic Aerodynamic and Aeroelastic Calculations about Airfoils and Wings
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781725624498
Category :
Languages : en
Pages : 36
Book Description
The development and application of transonic small disturbance codes for computing two dimensional flows, using the code ATRAN2, and for computing three dimensional flows, using the code ATRAN3S, are described. Calculated and experimental results are compared for unsteady flows about airfoils and wings, including several of the cases from the AGARD Standard Aeroelastic Configurations. In two dimensions, the results include AGARD priority cases for the NACA 64A006, NACA 64A010, NACA 0012, and MBB-A3 airfoils. In three dimensions, the results include flows about the F-5 wing, a typical wing, and the AGARD rectangular wings. Viscous corrections are included in some calculations, including those for the AGARD rectangular wing. For several cases, the aerodynamic and aeroelastic calculations are compared with experimental results. Goorjian, P. M. and Guruswamy, G. P. Ames Research Center NASA-TM-85986, A-9822, NAS 1.15:85986 RTOP 505-31-01...
Publisher: Createspace Independent Publishing Platform
ISBN: 9781725624498
Category :
Languages : en
Pages : 36
Book Description
The development and application of transonic small disturbance codes for computing two dimensional flows, using the code ATRAN2, and for computing three dimensional flows, using the code ATRAN3S, are described. Calculated and experimental results are compared for unsteady flows about airfoils and wings, including several of the cases from the AGARD Standard Aeroelastic Configurations. In two dimensions, the results include AGARD priority cases for the NACA 64A006, NACA 64A010, NACA 0012, and MBB-A3 airfoils. In three dimensions, the results include flows about the F-5 wing, a typical wing, and the AGARD rectangular wings. Viscous corrections are included in some calculations, including those for the AGARD rectangular wing. For several cases, the aerodynamic and aeroelastic calculations are compared with experimental results. Goorjian, P. M. and Guruswamy, G. P. Ames Research Center NASA-TM-85986, A-9822, NAS 1.15:85986 RTOP 505-31-01...
AGARD Two-dimensional Aeroelastic Configurations
Author: Samuel R. Bland
Publisher:
ISBN: 9789283513339
Category : Aerodynamics
Languages : en
Pages : 10
Book Description
The aeroelastician needs reliable efficient methods for the calculation of unsteady aerodynamic forces in the frequency critical transonic speed regime. The development of such methods can be enhanced by the availability of a limited number of test cases for the comparison of competing methods. This report contains such test cases. Geometric descriptions of seven, two-dimensional airfoils and suggested aerodynamic conditions for each are included. (Author).
Publisher:
ISBN: 9789283513339
Category : Aerodynamics
Languages : en
Pages : 10
Book Description
The aeroelastician needs reliable efficient methods for the calculation of unsteady aerodynamic forces in the frequency critical transonic speed regime. The development of such methods can be enhanced by the availability of a limited number of test cases for the comparison of competing methods. This report contains such test cases. Geometric descriptions of seven, two-dimensional airfoils and suggested aerodynamic conditions for each are included. (Author).
Introduction to Unsteady Aerodynamics and Dynamic Aeroelasticity
Author: Luciano Demasi
Publisher: Springer Nature
ISBN: 3031500547
Category :
Languages : en
Pages : 804
Book Description
Publisher: Springer Nature
ISBN: 3031500547
Category :
Languages : en
Pages : 804
Book Description
Calculation of Unsteady Transonic Flows with Mild Separation by Viscous-inviscid Interaction
Author: James T. Howlett
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 44
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 44
Book Description
NASA Technical Paper
Author:
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 132
Book Description
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 132
Book Description
Data from AGARD Report 702
Author: ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT NEUILLY-SUR-SEINE (France)
Publisher:
ISBN:
Category :
Languages : en
Pages : 16
Book Description
In the late seventies a need was perceived for standard comparison cases and experimental data to aid the comparison and validation of the theoretical methods then emerging for unsteady aerodynamics. A Working Group of the AGARD Structures and Materials panel chose a set of 2-D and 3-D configurations and for each configuration defined a set of test cases, including a priority subset, to be used for comparisons. These test cases were fully identified in ref. 1 and 2. The chosen configurations were known as the AGARD Aeroelastic Configurations and the chosen cases were denoted as Computational Test (CT) cases. Some of the CT cases were entirely theoretical while others were also the subject of unsteady measurements. The next step undertaken to aid the methods development was to produce an experimental data compendium (AGARD Report 702, ref. 3) which was conceived with the idea of bringing together the experimental data most important for the comparisons. The report was followed by an Addendum, ref. 4, which introduced two additional 3-D experiments. These reports established an admirable control base for providing experimental data and their value has been demonstrated by the repeated use of the test cases for the entire period since publication. The report has served as a model for the present new compendium of experimental data. It was decided that some of the data cases in the original Report 702 should be reproduced in this document in order to provide more complete coverage in this report with the additional bonus of making available the original data in electronic form to facilitate its continued use to validate calculations.
Publisher:
ISBN:
Category :
Languages : en
Pages : 16
Book Description
In the late seventies a need was perceived for standard comparison cases and experimental data to aid the comparison and validation of the theoretical methods then emerging for unsteady aerodynamics. A Working Group of the AGARD Structures and Materials panel chose a set of 2-D and 3-D configurations and for each configuration defined a set of test cases, including a priority subset, to be used for comparisons. These test cases were fully identified in ref. 1 and 2. The chosen configurations were known as the AGARD Aeroelastic Configurations and the chosen cases were denoted as Computational Test (CT) cases. Some of the CT cases were entirely theoretical while others were also the subject of unsteady measurements. The next step undertaken to aid the methods development was to produce an experimental data compendium (AGARD Report 702, ref. 3) which was conceived with the idea of bringing together the experimental data most important for the comparisons. The report was followed by an Addendum, ref. 4, which introduced two additional 3-D experiments. These reports established an admirable control base for providing experimental data and their value has been demonstrated by the repeated use of the test cases for the entire period since publication. The report has served as a model for the present new compendium of experimental data. It was decided that some of the data cases in the original Report 702 should be reproduced in this document in order to provide more complete coverage in this report with the additional bonus of making available the original data in electronic form to facilitate its continued use to validate calculations.
Current Status of Computational Methods for Transonic Unsteady Aerodynamics and Aeroelastic Applications
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 30
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 30
Book Description
Transonic Unsteady Aerodynamics and Aeroelasticity, 1987
Author:
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 684
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 684
Book Description
Computational Unsteady Aerodynamics for Aeroelastic Analysis
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 32
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 32
Book Description