Author: Florentino Idosor
Publisher:
ISBN:
Category : Rotors
Languages : en
Pages : 168
Book Description
Comparison of NASTRAN Analysis with Ground Vibration Results of UH-60A NASA/AEFA Test Configuration
Author: Florentino Idosor
Publisher:
ISBN:
Category : Rotors
Languages : en
Pages : 168
Book Description
Publisher:
ISBN:
Category : Rotors
Languages : en
Pages : 168
Book Description
Comparison of Nastran Analysis with Ground Vibration Results of Uh-60a Nasa/Aefa Test Configuration
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722970437
Category :
Languages : en
Pages : 102
Book Description
Preceding program flight tests, a ground vibration test and modal test analysis of a UH-60A Black Hawk helicopter was conducted by Sikorsky Aircraft to complement the UH-60A test plan and NASA/ARMY Modern Technology Rotor Airloads Program. The 'NASA/AEFA' shake test configuration was tested for modal frequencies and shapes and compared with its NASTRAN finite element model counterpart to give correlative results. Based upon previous findings, significant differences in modal data existed and were attributed to assumptions regarding the influence of secondary structure contributions in the preliminary NASTRAN modeling. An analysis of an updated finite element model including several secondary structural additions has confirmed that the inclusion of specific secondary components produces a significant effect on modal frequency and free-response shapes and improves correlations at lower frequencies with shake test data. Idosor, Florentino and Seible, Frieder Unspecified Center FINITE ELEMENT METHOD; GROUND TESTS; MATHEMATICAL MODELS; NASTRAN; STRUCTURAL ANALYSIS; UH-60A HELICOPTER; VIBRATION TESTS; AERODYNAMIC LOADS; AIRCRAFT STRUCTURES; ROTORS...
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722970437
Category :
Languages : en
Pages : 102
Book Description
Preceding program flight tests, a ground vibration test and modal test analysis of a UH-60A Black Hawk helicopter was conducted by Sikorsky Aircraft to complement the UH-60A test plan and NASA/ARMY Modern Technology Rotor Airloads Program. The 'NASA/AEFA' shake test configuration was tested for modal frequencies and shapes and compared with its NASTRAN finite element model counterpart to give correlative results. Based upon previous findings, significant differences in modal data existed and were attributed to assumptions regarding the influence of secondary structure contributions in the preliminary NASTRAN modeling. An analysis of an updated finite element model including several secondary structural additions has confirmed that the inclusion of specific secondary components produces a significant effect on modal frequency and free-response shapes and improves correlations at lower frequencies with shake test data. Idosor, Florentino and Seible, Frieder Unspecified Center FINITE ELEMENT METHOD; GROUND TESTS; MATHEMATICAL MODELS; NASTRAN; STRUCTURAL ANALYSIS; UH-60A HELICOPTER; VIBRATION TESTS; AERODYNAMIC LOADS; AIRCRAFT STRUCTURES; ROTORS...
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 244
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 244
Book Description
NASA's University Program Active Projects
Author:
Publisher:
ISBN:
Category : Federal aid to research
Languages : en
Pages : 510
Book Description
Publisher:
ISBN:
Category : Federal aid to research
Languages : en
Pages : 510
Book Description
Monthly Catalogue, United States Public Documents
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 950
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 950
Book Description
Monthly Catalog of United States Government Publications
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages :
Book Description
NASA SP.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 654
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 654
Book Description
The Modern Rotor Aerodynamic Limits Survey
Author: J. Cross
Publisher:
ISBN:
Category : Rotors
Languages : en
Pages : 280
Book Description
Publisher:
ISBN:
Category : Rotors
Languages : en
Pages : 280
Book Description
Aeronautical Engineering: A Cumulative Index to a Continuing Bibliography (supplement 274)
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 648
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 648
Book Description
Government Reports Announcements & Index
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 1092
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 1092
Book Description