Subsonic Flutter Characteristics of a Variable Sweep Wing and Horizontal Tail Combination

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ISBN 13 :
Total Pages : 112 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Subsonic Flutter Characteristics of a Variable Sweep Wing and Horizontal Tail Combination by : Walter J. Mykytow

Download or read book Subsonic Flutter Characteristics of a Variable Sweep Wing and Horizontal Tail Combination written by Walter J. Mykytow and published by . This book was released on 1970 with total page 112 pages. Available in PDF, EPUB and Kindle. Book excerpt: The project concerns a subsonic investigation of a new type of flutter phenomenon, not previously critical from a design standpoint, involving elastic modes of the wing, fuselage, and stabilizer combination and also involving aerodynamic interference between the wing and horizontal tail. The effort, consisting of design of a flutter model, vibration and subsonic wind tunnel tests, and flutter analyses, was conducted to determine important controlling flutter parameters, to evaluate the accuracy of analyses for predicting the phenomenon, to establish flutter trends and to define flutter prevention design criteria which could be used in the early design stage to avoid the problem. Some of the important features that were determined are increasing wing sweep can lead to lower flutter speeds; wing bending to fuselage torsion frequency ratios were defined which provide the mechanical coupling essential to produce the phenomenon and minimum flutter speeds as a function of wing sweep angle; vertical separation or dihedral angle can be very influential and beneficial and is more important than longitudinal separation, the effects of which were found to be small to moderate; the effects of compressibility have been shown to be detrimental and decrease the flutter speed, and conclusive proof that the interference aerodynamics between the wind and tail, and particularly, the downwash shed from the wing, is an important and detrimental feature to the phenomenon. (Author).

An Investigation of the Flutter Characteristics of Swept Wings at Subsonic Speeds

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ISBN 13 :
Total Pages : 143 pages
Book Rating : 4.:/5 (115 download)

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Book Synopsis An Investigation of the Flutter Characteristics of Swept Wings at Subsonic Speeds by : H. W. Hannah

Download or read book An Investigation of the Flutter Characteristics of Swept Wings at Subsonic Speeds written by H. W. Hannah and published by . This book was released on 1948 with total page 143 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Comparisons of Some Wing Flutter Characteristics Obtained by Modified Strip Analysis, Subsonic Kernel Function, and Experiment

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ISBN 13 :
Total Pages : 62 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Comparisons of Some Wing Flutter Characteristics Obtained by Modified Strip Analysis, Subsonic Kernel Function, and Experiment by : Edward Carson Yates

Download or read book Comparisons of Some Wing Flutter Characteristics Obtained by Modified Strip Analysis, Subsonic Kernel Function, and Experiment written by Edward Carson Yates and published by . This book was released on 1964 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Flutter Characteristics of Swept Wings at Transonic Speeds

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ISBN 13 :
Total Pages : 20 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Flutter Characteristics of Swept Wings at Transonic Speeds by : Laurence K. Loftin

Download or read book Flutter Characteristics of Swept Wings at Transonic Speeds written by Laurence K. Loftin and published by . This book was released on 1955 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:

The Effects at Subsonic Speeds of Wing Fences and a Tail on the Longitudinal Characteristics of a 63 Degree Swept-wing and Fuselage Combination

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ISBN 13 :
Total Pages : 38 pages
Book Rating : 4.:/5 (11 download)

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Book Synopsis The Effects at Subsonic Speeds of Wing Fences and a Tail on the Longitudinal Characteristics of a 63 Degree Swept-wing and Fuselage Combination by : Donald A. Buell

Download or read book The Effects at Subsonic Speeds of Wing Fences and a Tail on the Longitudinal Characteristics of a 63 Degree Swept-wing and Fuselage Combination written by Donald A. Buell and published by . This book was released on 1957 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Flutter Testing Techniques

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ISBN 13 :
Total Pages : 534 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Flutter Testing Techniques by :

Download or read book Flutter Testing Techniques written by and published by . This book was released on 1976 with total page 534 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Flutter Analysis of Swept-wing Subsonic Aircraft with Parameter Studies of Composite Wings

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ISBN 13 :
Total Pages : 116 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Flutter Analysis of Swept-wing Subsonic Aircraft with Parameter Studies of Composite Wings by : Jerrold M. Housner

Download or read book Flutter Analysis of Swept-wing Subsonic Aircraft with Parameter Studies of Composite Wings written by Jerrold M. Housner and published by . This book was released on 1974 with total page 116 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Use of Experimental Steady-flow Aerodynamic Parameters in the Calculation of Flutter Characteristics for Finite-span Swept Or Unswept Wings at Subsonic, Transonic, and Supersonic Speed

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ISBN 13 :
Total Pages : 58 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Use of Experimental Steady-flow Aerodynamic Parameters in the Calculation of Flutter Characteristics for Finite-span Swept Or Unswept Wings at Subsonic, Transonic, and Supersonic Speed by : Edward Carson Yates

Download or read book Use of Experimental Steady-flow Aerodynamic Parameters in the Calculation of Flutter Characteristics for Finite-span Swept Or Unswept Wings at Subsonic, Transonic, and Supersonic Speed written by Edward Carson Yates and published by . This book was released on 1960 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Prediction of Downwash Behind Swept-wing Airplanes at Subsonic Speed

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ISBN 13 :
Total Pages : 688 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Prediction of Downwash Behind Swept-wing Airplanes at Subsonic Speed by : John DeYoung

Download or read book Prediction of Downwash Behind Swept-wing Airplanes at Subsonic Speed written by John DeYoung and published by . This book was released on 1955 with total page 688 pages. Available in PDF, EPUB and Kindle. Book excerpt: A rapid method for estimating the downwash behind swept-wing airplanes is presented. The basic assumption is that of a flat horizontal sheet of vortices trailing behind the wing. The integrations for the downwash are handled in a manner similar to both Multhopp's and Weissinger's approximate integrations in their span-loading calculations. The principal effects of rolling-up of the wake are treated as corrections to the flat-sheet wake. A simple approximate correction for the effect of the fuselage is applied. The agreement with available experimental data taken behind airplane models is good. Computing forms are included together with charts of pertinent functions, so as to enable simple direct application.

Investigation of the Subsonic Flutter Characteristics of a Highly Swept Arrow Planform Wing with and Without Simulated Trailing-edge-mounted Engine Masses

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ISBN 13 :
Total Pages : 168 pages
Book Rating : 4.:/5 (216 download)

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Book Synopsis Investigation of the Subsonic Flutter Characteristics of a Highly Swept Arrow Planform Wing with and Without Simulated Trailing-edge-mounted Engine Masses by : Gerald David Walberg

Download or read book Investigation of the Subsonic Flutter Characteristics of a Highly Swept Arrow Planform Wing with and Without Simulated Trailing-edge-mounted Engine Masses written by Gerald David Walberg and published by . This book was released on 1962 with total page 168 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Scientific and Technical Aerospace Reports

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ISBN 13 :
Total Pages : 1280 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 1980 with total page 1280 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 : 818 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 1954 with total page 818 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Keywords Index to U.S. Government Technical Reports

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ISBN 13 :
Total Pages : 1160 pages
Book Rating : 4.3/5 (243 download)

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Book Synopsis Keywords Index to U.S. Government Technical Reports by :

Download or read book Keywords Index to U.S. Government Technical Reports written by and published by . This book was released on 1962 with total page 1160 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Keywords Index to U.S. Government Technical Reports (permuted Title Index).

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ISBN 13 :
Total Pages : 836 pages
Book Rating : 4.E/5 ( download)

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Book Synopsis Keywords Index to U.S. Government Technical Reports (permuted Title Index). by : United States. Department of Commerce. Office of Technical Services

Download or read book Keywords Index to U.S. Government Technical Reports (permuted Title Index). written by United States. Department of Commerce. Office of Technical Services and published by . This book was released on 1963 with total page 836 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Flutter Studies of Simplified Component Models of a Variable-sweep-wing Airplane at Mach Numbers Up to 3.0

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

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Book Synopsis Flutter Studies of Simplified Component Models of a Variable-sweep-wing Airplane at Mach Numbers Up to 3.0 by : Maynard C. Sandford

Download or read book Flutter Studies of Simplified Component Models of a Variable-sweep-wing Airplane at Mach Numbers Up to 3.0 written by Maynard C. Sandford and published by . This book was released on 1966 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Some Effects of Variations in Density and Aerodynamic Parameters on the Calculated Flutter Characteristics of Finite-span Swept and Unswept Wings at Subsonic and Supersonic Speeds

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ISBN 13 :
Total Pages : 134 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Some Effects of Variations in Density and Aerodynamic Parameters on the Calculated Flutter Characteristics of Finite-span Swept and Unswept Wings at Subsonic and Supersonic Speeds by : Edward Carson Yates

Download or read book Some Effects of Variations in Density and Aerodynamic Parameters on the Calculated Flutter Characteristics of Finite-span Swept and Unswept Wings at Subsonic and Supersonic Speeds written by Edward Carson Yates and published by . This book was released on 1960 with total page 134 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Effects of Wing-body Geometry on the Lateral-flow Angularities at Subsonic Speeds

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ISBN 13 :
Total Pages : 28 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Effects of Wing-body Geometry on the Lateral-flow Angularities at Subsonic Speeds by : Frank S. Malvestuto

Download or read book Effects of Wing-body Geometry on the Lateral-flow Angularities at Subsonic Speeds written by Frank S. Malvestuto and published by . This book was released on 1956 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: The lateral flow characteristics in the region of a vertical tail have been investigated experimentally and theoretically at low subsonic speeds. The effects of changes in wing-body geometry such as nose position and shape, fuselage cross-sectional shape, and wing vertical position are described. The theoretical model which approximates the separated flow phenomena by a simple cylinder-vortex flow is described in an appendix.