Identification of Longitudinal Aerodynamic and Handling Qualities Parameters of the X-31A Aircraft from Flight Test Data

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ISBN 13 :
Total Pages : 136 pages
Book Rating : 4.:/5 (361 download)

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Book Synopsis Identification of Longitudinal Aerodynamic and Handling Qualities Parameters of the X-31A Aircraft from Flight Test Data by : Luong Van Nguyen

Download or read book Identification of Longitudinal Aerodynamic and Handling Qualities Parameters of the X-31A Aircraft from Flight Test Data written by Luong Van Nguyen and published by . This book was released on 1996 with total page 136 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Longitudinal Aerodynamics Extracted from Flight Tests Using a Parameter Estimation Method

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ISBN 13 : 9780642905932
Total Pages : 28 pages
Book Rating : 4.9/5 (59 download)

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Book Synopsis Longitudinal Aerodynamics Extracted from Flight Tests Using a Parameter Estimation Method by : R. A. Feik

Download or read book Longitudinal Aerodynamics Extracted from Flight Tests Using a Parameter Estimation Method written by R. A. Feik and published by . This book was released on 1978 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: Flight data from a 60 deg. delta wing aircraft have been analysed using a modified Newton-Raphson parameter estimation procedure. The model equations used for the analysis were extended to account for incidence vane errors and non-linearities in the pitching moment curves. Longitudinal derivatives extracted from the data have been compared with wind tunnel measurements and some theoretical estimates and areas of agreement and disagreement identified. The results demonstrate the usefulness of the parameter identification method not only for the validation of aircraft mathematical models and for checking flight results against wind tunnel data but also for obtaining aerodynamic data not easily available through other means. (Author).

Lateral and Longitudinal Aerodynamic Stability and Control Parameters of the Basic Vortex Flap Research Aircraft as Determined from Flight Test Data

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ISBN 13 :
Total Pages : 42 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Lateral and Longitudinal Aerodynamic Stability and Control Parameters of the Basic Vortex Flap Research Aircraft as Determined from Flight Test Data by :

Download or read book Lateral and Longitudinal Aerodynamic Stability and Control Parameters of the Basic Vortex Flap Research Aircraft as Determined from Flight Test Data written by and published by . This book was released on 1986 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Evaluation of High-angle-of-attack Handling Qualities for the X-31A Using Standard Evaluation Maneuvers

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ISBN 13 :
Total Pages : 32 pages
Book Rating : 4.:/5 (73 download)

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Book Synopsis Evaluation of High-angle-of-attack Handling Qualities for the X-31A Using Standard Evaluation Maneuvers by : P. C. Stoliker

Download or read book Evaluation of High-angle-of-attack Handling Qualities for the X-31A Using Standard Evaluation Maneuvers written by P. C. Stoliker and published by . This book was released on 1996 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: The X-31A aircraft gross-acquisition and fine-tracking handling qualities have been evaluated using standard evaluation maneuvers developed by Wright Laboratory, Wright-Patterson Air Force Base. The emphasis of the testing is in the angle-of-attack range between 30° and 70°. Longitudinal gross-acquisition handling qualities results show borderline Level 1/Level 2 performance. Lateral gross-acquisition testing results in Level 1/Level 2 ratings below 45° angle of attack, degrading into Level 3 as angle of attack increases. The fine-tracking performance in both longitudinal and lateral axes also receives Level 1 ratings near 30° angle of attack, with the ratings tending towards Level 3 at angles of attack greater than 50°. These ratings do not match the expectations from the extensive close-in combat testing where the X-31A aircraft demonstrated fair to good handling qualities maneuvering for high angles of attack. This paper presents the results of the high-angle-of-attack handling qualities flight testing of the X-31A aircraft. Discussion of the preparation for the maneuvers, the pilot ratings, and selected pilot comments are included. Evaluation of the results is made in conjunction with existing Neal-Smith, bandwidth, Smith-Geddes, and military specifications.

Linearized Poststall Aerodynamic and Control Law Models of the X-31a Aircraft and Comparison with Flight Data

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Publisher : Createspace Independent Publishing Platform
ISBN 13 : 9781722616151
Total Pages : 66 pages
Book Rating : 4.6/5 (161 download)

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Book Synopsis Linearized Poststall Aerodynamic and Control Law Models of the X-31a Aircraft and Comparison with Flight Data by : National Aeronautics and Space Administration (NASA)

Download or read book Linearized Poststall Aerodynamic and Control Law Models of the X-31a Aircraft and Comparison with Flight Data written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-08 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt: The X-31A aircraft has a unique configuration that uses thrust-vector vanes and aerodynamic control effectors to provide an operating envelope to a maximum 70 deg angle of attack, an inherently nonlinear portion of the flight envelope. This report presents linearized versions of the X-31A longitudinal and lateral-directional control systems, with aerodynamic models sufficient to evaluate characteristics in the poststall envelope at 30 deg, 45 deg, and 60 deg angle of attack. The models are presented with detail sufficient to allow the reader to reproduce the linear results or perform independent control studies. Comparisons between the responses of the linear models and flight data are presented in the time and frequency domains to demonstrate the strengths and weaknesses of the ability to predict high-angle-of-attack flight dynamics using linear models. The X-31A six-degree-of-freedom simulation contains a program that calculates linear perturbation models throughout the X-31A flight envelope. The models include aerodynamics and flight control system dynamics that are used for stability, controllability, and handling qualities analysis. The models presented in this report demonstrate the ability to provide reasonable linear representations in the poststall flight regime. Stoliker, Patrick C. and Bosworth, John T. and Georgie, Jennifer Armstrong Flight Research Center...

Linearized Aerodynamic and Control Law Models of the X-29A Airplane and Comparison with Flight Data

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ISBN 13 :
Total Pages : 120 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Linearized Aerodynamic and Control Law Models of the X-29A Airplane and Comparison with Flight Data by : John T. Bosworth

Download or read book Linearized Aerodynamic and Control Law Models of the X-29A Airplane and Comparison with Flight Data written by John T. Bosworth and published by . This book was released on 1992 with total page 120 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Scientific and Technical Aerospace Reports

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ISBN 13 :
Total Pages : 702 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Scientific and Technical Aerospace Reports by :

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 702 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic-derivative Characteristics of the X-15 Research Airplane as Determined from Flight Tests for Mach Numbers from 0.6 to 3.4

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ISBN 13 :
Total Pages : 72 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Aerodynamic-derivative Characteristics of the X-15 Research Airplane as Determined from Flight Tests for Mach Numbers from 0.6 to 3.4 by : Roxanah B. Yancey

Download or read book Aerodynamic-derivative Characteristics of the X-15 Research Airplane as Determined from Flight Tests for Mach Numbers from 0.6 to 3.4 written by Roxanah B. Yancey and published by . This book was released on 1962 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Technical Publications Announcements with Indexes

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ISBN 13 :
Total Pages : 1318 pages
Book Rating : 4.:/5 (319 download)

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Book Synopsis Technical Publications Announcements with Indexes by : United States. National Aeronautics and Space Administration

Download or read book Technical Publications Announcements with Indexes written by United States. National Aeronautics and Space Administration and published by . This book was released on 1962 with total page 1318 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Scientific and Technical Reports

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ISBN 13 :
Total Pages : 1440 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis NASA Scientific and Technical Reports by : United States. National Aeronautics and Space Administration Scientific and Technical Information Division

Download or read book NASA Scientific and Technical Reports written by United States. National Aeronautics and Space Administration Scientific and Technical Information Division and published by . This book was released on 1966 with total page 1440 pages. Available in PDF, EPUB and Kindle. Book excerpt:

International Aerospace Abstracts

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ISBN 13 :
Total Pages : 512 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis International Aerospace Abstracts by :

Download or read book International Aerospace Abstracts written by and published by . This book was released on 1996 with total page 512 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Selected Listing of NASA Scientific and Technical Reports for ...

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ISBN 13 :
Total Pages : 388 pages
Book Rating : 4.X/5 (4 download)

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Book Synopsis A Selected Listing of NASA Scientific and Technical Reports for ... by :

Download or read book A Selected Listing of NASA Scientific and Technical Reports for ... written by and published by . This book was released on 1957 with total page 388 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Longitudinal Aerodynamic Parameters Fo the Kestrel Aircraft, XV-6A, Extracted from Flight Data

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ISBN 13 :
Total Pages : 50 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Longitudinal Aerodynamic Parameters Fo the Kestrel Aircraft, XV-6A, Extracted from Flight Data by : James L. Williams

Download or read book Longitudinal Aerodynamic Parameters Fo the Kestrel Aircraft, XV-6A, Extracted from Flight Data written by James L. Williams and published by . This book was released on 1973 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Guide to Annual Subject Index for Technical Publications Announcements, Apr.-Dec. 1962

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ISBN 13 :
Total Pages : 720 pages
Book Rating : 4.:/5 (318 download)

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Book Synopsis Guide to Annual Subject Index for Technical Publications Announcements, Apr.-Dec. 1962 by : United States. National Aeronautics and Space Administration

Download or read book Guide to Annual Subject Index for Technical Publications Announcements, Apr.-Dec. 1962 written by United States. National Aeronautics and Space Administration and published by . This book was released on 1962 with total page 720 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aeronautical Engineering

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ISBN 13 :
Total Pages : 538 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Aeronautical Engineering by :

Download or read book Aeronautical Engineering written by and published by . This book was released on 1991 with total page 538 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Design Procedure for the Handling Qualities Optimization of the X-29A Aircraft

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ISBN 13 :
Total Pages : 28 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis A Design Procedure for the Handling Qualities Optimization of the X-29A Aircraft by : John T. Bosworth

Download or read book A Design Procedure for the Handling Qualities Optimization of the X-29A Aircraft written by John T. Bosworth and published by . This book was released on 1989 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Index of NACA Technical Publications

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ISBN 13 :
Total Pages : 388 pages
Book Rating : 4.:/5 (2 download)

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Book Synopsis Index of NACA Technical Publications by : United States. National Advisory Committee for Aeronautics

Download or read book Index of NACA Technical Publications written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1959 with total page 388 pages. Available in PDF, EPUB and Kindle. Book excerpt: