Dynamic Structural Aeroelastic Stability Testing of the XV-15 Tilt Rotor Research Aircraft PDF Download
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Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 26
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Book Description
For the past 20 years, a significant effort has been made to understand and predict the structural aeroelastic stability characteristics of the tilt rotor concept. Beginning with the rotor-pylon oscillation of the XV-3 aircraft, and the problem was identified and then subjected to a series of theoretical studies, plus model and full-scale wind tunnel tests. From this data base, methods were developed to predict the structural aeroelastic stability characteristics of the XV-15 Tilt Rotor Research Aircraft. This paper examines the predicted aeroelastic characteristics in light of the major parameters effecting rotor-pylon-wing stability; describes flight test techniques used to obtain XV-15 aeroelastic stability; presents a summary of flight test results; compares the flight test results to the predicted values; and presents a limited comparison of wind tunnel results, flight test results, and their correlation with predicted values.
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 26
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Book Description
For the past 20 years, a significant effort has been made to understand and predict the structural aeroelastic stability characteristics of the tilt rotor concept. Beginning with the rotor-pylon oscillation of the XV-3 aircraft, and the problem was identified and then subjected to a series of theoretical studies, plus model and full-scale wind tunnel tests. From this data base, methods were developed to predict the structural aeroelastic stability characteristics of the XV-15 Tilt Rotor Research Aircraft. This paper examines the predicted aeroelastic characteristics in light of the major parameters effecting rotor-pylon-wing stability; describes flight test techniques used to obtain XV-15 aeroelastic stability; presents a summary of flight test results; compares the flight test results to the predicted values; and presents a limited comparison of wind tunnel results, flight test results, and their correlation with predicted values.
Author: Martin D. Maisel
Publisher:
ISBN:
Category : Transportation
Languages : en
Pages : 226
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Book Description
Author: Martin D. Maisel
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 222
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Book Description
Author: Wayne Johnson
Publisher:
ISBN:
Category : Rotors (Helicopters)
Languages : en
Pages : 32
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Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 32
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Book Description
Author:
Publisher: DIANE Publishing
ISBN: 1428995803
Category :
Languages : en
Pages : 115
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Book Description
Author:
Publisher: DIANE Publishing
ISBN: 1428916830
Category :
Languages : en
Pages : 34
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Book Description
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 32
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Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 28
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Book Description
Author: ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT NEUILLY-SUR-SEINE (France)
Publisher:
ISBN:
Category :
Languages : en
Pages : 539
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Book Description
Contents: Conclusions of the FMP Symposium in Valloire (1975) and Progress on Ground/Fight Correlation; Progress in Wind Tunnel Test Techniques and in the Corrections and Analysis of the Results; Ground/Flight Correlation on the Space Shuttle Orbiter from Re-Entry to Landing; Ground/Flight Correlation on the Alpha-Jet Experimental Aircraft with a Transonic Wing; Flight and Wind-Tunnel Correlation of Boundary-Layer Transition on the AEDC Transition Cone; Experimental Investigations of Transport Aircraft Low Speed Engine Interference Effects and Flight Test Correlation; Comparison of Prediction, Wind Tunnel and Flight Test Data for the Canadair Challenger Turbofan Aircraft; Lessons from Tornado Afterbody Development; The Use of Free-Flight Models for the Prediction of Departure Control; Comparison of Flight and Wind Tunnel Buffeting Measurements on the SAAB 105 Aircraft; Some Measurements of Buffeting on a Flutter Model of a Typical Strike Aircraft; Correlation Aspects of Analytical Wind Tunnel and Flight Test Results for a Hingeless Rotor Helicopter; Dynamic Structural Aeroelastic Stability Testing of the XV-15 Tilt Rotor Research Aircraft; Structural Aspects of Ground/Flight Correlation on the Variable Sweep Wing Aircraft Tornado; Real-Time Flutter Analysis of an Active Flutter-Suppression System on a Remotely Piloted Research Aircraft; Flight Flutter Testing with Emphasis on the Tip Vane Method.
