The Effects of Sideslip, Aspect Ratio, and Mach Number on the Lift and Pitching Moment of Triangular, Trapezoidal, and Related Plan Forms in Supersonic Flow

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Total Pages : 78 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis The Effects of Sideslip, Aspect Ratio, and Mach Number on the Lift and Pitching Moment of Triangular, Trapezoidal, and Related Plan Forms in Supersonic Flow by : Arthur L. Jones

Download or read book The Effects of Sideslip, Aspect Ratio, and Mach Number on the Lift and Pitching Moment of Triangular, Trapezoidal, and Related Plan Forms in Supersonic Flow written by Arthur L. Jones and published by . This book was released on 1949 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt: The variations of lift and pitching moment with sideslip in supersonic flow have been calculated for a representative gorup of plan forms. The variations of lift and pitching moment with aspect ratio and Mach number at zero sideslip were also investigated. The analysis was based on linearized potential theory and was applied to triangular, trapezoidal, rectangular, and swept-back plan forms without dihedral.

Technical Note - National Advisory Committee for Aeronautics

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ISBN 13 :
Total Pages : 1190 pages
Book Rating : 4.E/5 ( download)

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Book Synopsis Technical Note - National Advisory Committee for Aeronautics by : United States. National Advisory Committee for Aeronautics

Download or read book Technical Note - National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1951 with total page 1190 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Elevated-temperature Properties of Several Titanium Carbide Base Ceramals

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ISBN 13 :
Total Pages : 694 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Elevated-temperature Properties of Several Titanium Carbide Base Ceramals by : George C. Deutsch

Download or read book Elevated-temperature Properties of Several Titanium Carbide Base Ceramals written by George C. Deutsch and published by . This book was released on 1949 with total page 694 pages. Available in PDF, EPUB and Kindle. Book excerpt: On a strength-to-weight ratio basis, ceramals appeared promising as gas-turbine-blade materials in the temperature range of 1600 to 2400 degrees F.

Some Theoretical Characteristics of Trapezoidal Wings in Supersonic Flow and a Comparison of Several Wing-flap Combinations

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Total Pages : 32 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Some Theoretical Characteristics of Trapezoidal Wings in Supersonic Flow and a Comparison of Several Wing-flap Combinations by : Robert O. Piland

Download or read book Some Theoretical Characteristics of Trapezoidal Wings in Supersonic Flow and a Comparison of Several Wing-flap Combinations written by Robert O. Piland and published by . This book was released on 1951 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: The theoretical lift and pitching moment due to angle of attack and pitching and the lateral force and yawing moment due to rolling of a trapezoidal wing are derived. The equations are applicable when the inboard Mach line from a leading-edge tip intersects the trailing edge and the outboard Mach line lies ahead of the side edge. When the side edges are raked in, the former condition is sufficient. A comparison based on theoretical expressions of the lift and rolling effectiveness for half-delta tip (point forward) and trailing-edge flaps on various plan forms is made.

Bibliography of Technical Reports

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ISBN 13 :
Total Pages : 62 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Bibliography of Technical Reports by :

Download or read book Bibliography of Technical Reports written by and published by . This book was released on 1950 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Investigation of the Effects of Model Scale and Stream Reynolds Number on the Aerodynamic Characteristics of Two Rectangular Wings at Supersonic Speeds on the Langley 9-inch Supersonic Tunnel

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ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Investigation of the Effects of Model Scale and Stream Reynolds Number on the Aerodynamic Characteristics of Two Rectangular Wings at Supersonic Speeds on the Langley 9-inch Supersonic Tunnel by : Donald E. Coletti

Download or read book Investigation of the Effects of Model Scale and Stream Reynolds Number on the Aerodynamic Characteristics of Two Rectangular Wings at Supersonic Speeds on the Langley 9-inch Supersonic Tunnel written by Donald E. Coletti and published by . This book was released on 1955 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Application of the Laplace Transformation to the Solution of the Lateral and Longitudinal Stability Equations

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ISBN 13 :
Total Pages : 698 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Application of the Laplace Transformation to the Solution of the Lateral and Longitudinal Stability Equations by : Andrew Gustav Mokrzycki

Download or read book Application of the Laplace Transformation to the Solution of the Lateral and Longitudinal Stability Equations written by Andrew Gustav Mokrzycki and published by . This book was released on 1950 with total page 698 pages. Available in PDF, EPUB and Kindle. Book excerpt: The application of the Laplace transformation to the solution of the lateral and longitudinal stability equations is presented. The expressions for the time history of the motion in response to a sinusoidal control motion are derived for the general case in which the initial conditions, initial displacements and initial velocities, are assumed different from zero. Some illustrative examples of the application of the Laplace transform to ordinary linear differential equations with constant coefficients and a number example of a specific problem are presented in appendixes.

Technical Note

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ISBN 13 :
Total Pages : 440 pages
Book Rating : 4.3/5 (243 download)

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Book Synopsis Technical Note by : United States. National Advisory Committee for Aeronautics

Download or read book Technical Note written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1950 with total page 440 pages. Available in PDF, EPUB and Kindle. Book excerpt:

The Rolling Moment Due to Sideslip of Triangular, Trapezoidal, and Related Plan Forms in Supersonic Flow

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ISBN 13 :
Total Pages : 644 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis The Rolling Moment Due to Sideslip of Triangular, Trapezoidal, and Related Plan Forms in Supersonic Flow by : Arthur L. Jones

Download or read book The Rolling Moment Due to Sideslip of Triangular, Trapezoidal, and Related Plan Forms in Supersonic Flow written by Arthur L. Jones and published by . This book was released on 1948 with total page 644 pages. Available in PDF, EPUB and Kindle. Book excerpt: The variation of the rolling moment with sideslip and the variation of the derivative with aspect ratio and Mach number were investigated.

Applied Mechanics Reviews

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ISBN 13 :
Total Pages : 446 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Applied Mechanics Reviews by :

Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1948 with total page 446 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Monthly Catalog of United States Government Publications

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ISBN 13 :
Total Pages : 1878 pages
Book Rating : 4.3/5 (121 download)

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Book Synopsis Monthly Catalog of United States Government Publications by :

Download or read book Monthly Catalog of United States Government Publications written by and published by . This book was released on 1961 with total page 1878 pages. Available in PDF, EPUB and Kindle. Book excerpt:

United States Government Publications Monthly Catalog

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ISBN 13 :
Total Pages : 1138 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis United States Government Publications Monthly Catalog by :

Download or read book United States Government Publications Monthly Catalog written by and published by . This book was released on 1948-07 with total page 1138 pages. Available in PDF, EPUB and Kindle. Book excerpt:

List of Technical Notes, 1947-1953

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ISBN 13 :
Total Pages : 162 pages
Book Rating : 4.0/5 ( download)

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Book Synopsis List of Technical Notes, 1947-1953 by : United States. National Advisory Committee for Aeronautics

Download or read book List of Technical Notes, 1947-1953 written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1954 with total page 162 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Handbook of Supersonic Aerodynamics

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ISBN 13 :
Total Pages : 102 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Handbook of Supersonic Aerodynamics by : Johns Hopkins University. Applied Physics Laboratory

Download or read book Handbook of Supersonic Aerodynamics written by Johns Hopkins University. Applied Physics Laboratory and published by . This book was released on 1957 with total page 102 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Report

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ISBN 13 :
Total Pages : 46 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Report by : United States. National Advisory Committee for Aeronautics

Download or read book Report written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1951 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Report - National Advisory Committee for Aeronautics

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ISBN 13 :
Total Pages : 1462 pages
Book Rating : 4.E/5 ( download)

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Book Synopsis Report - National Advisory Committee for Aeronautics by : United States. National Advisory Committee for Aeronautics

Download or read book Report - National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1951 with total page 1462 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Experimental Determination of the Effect of Horizontal-tail Size, Tail Length, and Vertical Location on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45 ̊sweptback Wing and Tail Surfaces

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ISBN 13 :
Total Pages : 340 pages
Book Rating : 4.3/5 (243 download)

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Book Synopsis Experimental Determination of the Effect of Horizontal-tail Size, Tail Length, and Vertical Location on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45 ̊sweptback Wing and Tail Surfaces by : Arthur Earl Bryson

Download or read book Experimental Determination of the Effect of Horizontal-tail Size, Tail Length, and Vertical Location on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45 ̊sweptback Wing and Tail Surfaces written by Arthur Earl Bryson and published by . This book was released on 1952 with total page 340 pages. Available in PDF, EPUB and Kindle. Book excerpt: