Investigation of Methods for Computing Flutter Characteristics of Supersonic Delta Wings and Comparison with Experimental Data

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ISBN 13 :
Total Pages : 74 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Investigation of Methods for Computing Flutter Characteristics of Supersonic Delta Wings and Comparison with Experimental Data by : Charles Harold Wilts

Download or read book Investigation of Methods for Computing Flutter Characteristics of Supersonic Delta Wings and Comparison with Experimental Data written by Charles Harold Wilts and published by . This book was released on 1959 with total page 74 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Investigation of Methods for Computing Flutter Characteristics of Supersonic Delta Wings and Comparison with Experimental Data

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ISBN 13 :
Total Pages : 70 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Investigation of Methods for Computing Flutter Characteristics of Supersonic Delta Wings and Comparison with Experimental Data by : Charles Harold Wilts

Download or read book Investigation of Methods for Computing Flutter Characteristics of Supersonic Delta Wings and Comparison with Experimental Data written by Charles Harold Wilts and published by . This book was released on 1959 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Technical Note

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ISBN 13 :
Total Pages : 1018 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis NASA Technical Note by :

Download or read book NASA Technical Note written by and published by . This book was released on 1959 with total page 1018 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Flutter Analysis of Highly Swept Delta Wings by Conventional Methods

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ISBN 13 :
Total Pages : 24 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Flutter Analysis of Highly Swept Delta Wings by Conventional Methods by :

Download or read book Flutter Analysis of Highly Swept Delta Wings by Conventional Methods written by and published by . This book was released on 1988 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Flutter Analysis of Highly Swept Delta Wings by Conventional Methods

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Publisher : Independently Published
ISBN 13 : 9781792728488
Total Pages : 36 pages
Book Rating : 4.7/5 (284 download)

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Book Synopsis Flutter Analysis of Highly Swept Delta Wings by Conventional Methods by : National Aeronautics and Space Adm Nasa

Download or read book Flutter Analysis of Highly Swept Delta Wings by Conventional Methods written by National Aeronautics and Space Adm Nasa and published by Independently Published. This book was released on 2018-12-31 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: The flutter boundaries of six thin highly-swept delta-platform wings have been calculated. Comparisons are made between experimental data and results using several aerodynamic methods. The aerodynamic methods used include a subsonic and supersonic kernel function, second order piston theory, and a transonic small disturbance code. The dynamic equations of motion are solved using analytically calculated mode shapes and frequencies. Gibbons, M. D. and Soistmann, D. L. and Bennett, R. M. Langley Research Center NASA-TM-101530, NAS 1.15:101530 RTOP 505-63-21-01...

Procedure for Calculating Flutter at High Supersonic Speed Including Camber Deflections, and Comparisons with Experimental Results

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ISBN 13 :
Total Pages : 32 pages
Book Rating : 4.:/5 (692 download)

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Book Synopsis Procedure for Calculating Flutter at High Supersonic Speed Including Camber Deflections, and Comparisons with Experimental Results by : Homer G. Morgan

Download or read book Procedure for Calculating Flutter at High Supersonic Speed Including Camber Deflections, and Comparisons with Experimental Results written by Homer G. Morgan and published by . This book was released on 1958 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: The method is used to calculate the flutter speed of some wings which had been previously tested at Mach numbers of 1.3 to 3.0. Comparison of the calculations and experiment is made for flat-plate 60 degrees and 45 degrees delta wings and also for an untapered 45 degree sweptback wing.

Semiannual Report to the Congress

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ISBN 13 :
Total Pages : 302 pages
Book Rating : 4.3/5 ( download)

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Book Synopsis Semiannual Report to the Congress by : United States. National Aeronautics and Space Administration

Download or read book Semiannual Report to the Congress written by United States. National Aeronautics and Space Administration and published by . This book was released on 1959 with total page 302 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Shock and Vibration Environment

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ISBN 13 :
Total Pages : 162 pages
Book Rating : 4.E/5 ( download)

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Book Synopsis Shock and Vibration Environment by : Wendell L. Hercules

Download or read book Shock and Vibration Environment written by Wendell L. Hercules and published by . This book was released on 1962 with total page 162 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Index of NASA Technical Publications

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ISBN 13 :
Total Pages : 448 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Index of NASA Technical Publications by : United States. National Aeronautics and Space Administration

Download or read book Index of NASA Technical Publications written by United States. National Aeronautics and Space Administration and published by . This book was released on 1960 with total page 448 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Flutter at Very High Speeds

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ISBN 13 :
Total Pages : 16 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Flutter at Very High Speeds by : Harry L. Runyan

Download or read book Flutter at Very High Speeds written by Harry L. Runyan and published by . This book was released on 1957 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt: This paper is concerned with a discussion of some of the problems of flutter and aeroelasticity that are or may be important at high speeds. Various theoretical procedures for treating high Mach number flutter are reviewed. Application of two of these methods, namely, the Van Dyke method and piston-theory method, is made to a specific example and compared with linear two- and three-dimensional results. It is shown that the effects of thickness and airfoil shape are destabilizing as compared with linear theory at high Mach number. In order to demonstrate the validity of these large predicted effects, experimental flutter results are shown for two rectangular wings at Mach numbers of 6.86 and 3. The results of nonlinear piston-theory calculations were in good agreement with experiment, whereas the results of using two- and three-dimensional linear theory were not. In addition, some results demonstrating the importance of including camber modes in a flutter analysis are shown, as well as a discussion of one case of flutter due to aerodynamic heating.

Aeronautical Engineering

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ISBN 13 :
Total Pages : 580 pages
Book Rating : 4.F/5 ( 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 1971 with total page 580 pages. Available in PDF, EPUB and Kindle. Book excerpt: A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA)

Scientific and Technical Aerospace Reports

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ISBN 13 :
Total Pages : 892 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 1994 with total page 892 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Preliminary Wind-tunnel Investigation of Flutter Characteristics of Delta Wings

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ISBN 13 :
Total Pages : 40 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis A Preliminary Wind-tunnel Investigation of Flutter Characteristics of Delta Wings by : Robert W. Herr

Download or read book A Preliminary Wind-tunnel Investigation of Flutter Characteristics of Delta Wings written by Robert W. Herr and published by . This book was released on 1952 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:

The Journal of the Royal Aeronautical Society

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ISBN 13 :
Total Pages : 1110 pages
Book Rating : 4.:/5 (319 download)

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Book Synopsis The Journal of the Royal Aeronautical Society by : Royal Aeronautical Society

Download or read book The Journal of the Royal Aeronautical Society written by Royal Aeronautical Society and published by . This book was released on 1959 with total page 1110 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Technical Abstract Bulletin

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ISBN 13 :
Total Pages : 548 pages
Book Rating : 4.E/5 ( download)

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Book Synopsis Technical Abstract Bulletin by :

Download or read book Technical Abstract Bulletin written by and published by . This book was released on 1965 with total page 548 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Supersonic Flutter of a 60© Delta Wing Encountered During the Flight Test of a Rocket-propelled Model

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ISBN 13 :
Total Pages : 26 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Supersonic Flutter of a 60© Delta Wing Encountered During the Flight Test of a Rocket-propelled Model by : William T. Lauten

Download or read book Supersonic Flutter of a 60© Delta Wing Encountered During the Flight Test of a Rocket-propelled Model written by William T. Lauten and published by . This book was released on 1954 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt: An analysis of the flight time-history records of a record-propelled 60 degree delta-wing airplane configuration indicate that wing flutter started during the accelerating portion of the flight at a Mach number of approximately 1.7 and continued through the peak Mach number of the test (M = 2.08) and during deceleration at least until telemeter failure at M = 1.4 and probably to an even lower speed. CW Doppler velocimeter data indicated that the wings did not fail during the flight.

Index to NASA Technical Publications

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

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Book Synopsis Index to NASA Technical Publications by : United States. National Aeronautics and Space Administration

Download or read book Index to NASA Technical Publications written by United States. National Aeronautics and Space Administration and published by . This book was released on 1960-07 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: