Comparison of NASTRAN Analysis with Ground Vibration Results of UH-60A NASA/AEFA Test Configuration

Comparison of NASTRAN Analysis with Ground Vibration Results of UH-60A NASA/AEFA Test Configuration PDF Author: Florentino Idosor
Publisher:
ISBN:
Category : Rotors
Languages : en
Pages : 168

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Comparison of NASTRAN Analysis with Ground Vibration Results of UH-60A NASA/AEFA Test Configuration

Comparison of NASTRAN Analysis with Ground Vibration Results of UH-60A NASA/AEFA Test Configuration PDF Author: Florentino Idosor
Publisher:
ISBN:
Category : Rotors
Languages : en
Pages : 168

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Comparison of Nastran Analysis with Ground Vibration Results of Uh-60a Nasa/Aefa Test Configuration

Comparison of Nastran Analysis with Ground Vibration Results of Uh-60a Nasa/Aefa Test Configuration PDF Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722970437
Category :
Languages : en
Pages : 102

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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

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 244

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NASA's University Program Active Projects

NASA's University Program Active Projects PDF Author:
Publisher:
ISBN:
Category : Federal aid to research
Languages : en
Pages : 510

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Monthly Catalogue, United States Public Documents

Monthly Catalogue, United States Public Documents PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 950

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Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author:
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ISBN:
Category : Government publications
Languages : en
Pages :

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NASA SP.

NASA SP. PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 654

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The Modern Rotor Aerodynamic Limits Survey

The Modern Rotor Aerodynamic Limits Survey PDF Author: J. Cross
Publisher:
ISBN:
Category : Rotors
Languages : en
Pages : 280

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Aeronautical Engineering: A Cumulative Index to a Continuing Bibliography (supplement 274)

Aeronautical Engineering: A Cumulative Index to a Continuing Bibliography (supplement 274) PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 648

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Government Reports Announcements & Index

Government Reports Announcements & Index PDF Author:
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ISBN:
Category : Science
Languages : en
Pages : 1092

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