A Comparison At Mach Numbers Up To 092 Of The Calculated And Experimental Downwash And Wake Characteristics At Various Horizonatl Tail Heights Behind A Wing With 45 Degrees Of Sweepback PDF Download

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A Comparison at Mach Numbers Up to 0.92 of the Calculated and Experimental Downwash and Wake Characteristics at Various Horizonatl Tail Heights Behind a Wing with 45 Degrees of Sweepback

A Comparison at Mach Numbers Up to 0.92 of the Calculated and Experimental Downwash and Wake Characteristics at Various Horizonatl Tail Heights Behind a Wing with 45 Degrees of Sweepback
Author: Jack D. Stephenson
Publisher:
Total Pages: 86
Release: 1955
Genre: Aeronautics
ISBN:

Download A Comparison at Mach Numbers Up to 0.92 of the Calculated and Experimental Downwash and Wake Characteristics at Various Horizonatl Tail Heights Behind a Wing with 45 Degrees of Sweepback Book in PDF, ePub and Kindle


Comparison Between Experimental and Predicted Downwash at a Mach Number of 0.25 Behind a Wing-body Combination Having a Triangular Wing of Aspect Ratio 2.0

Comparison Between Experimental and Predicted Downwash at a Mach Number of 0.25 Behind a Wing-body Combination Having a Triangular Wing of Aspect Ratio 2.0
Author: Norman E. Sorenson
Publisher:
Total Pages: 29
Release: 1956
Genre: Airplanes
ISBN:

Download Comparison Between Experimental and Predicted Downwash at a Mach Number of 0.25 Behind a Wing-body Combination Having a Triangular Wing of Aspect Ratio 2.0 Book in PDF, ePub and Kindle

A study was undertaken to evaluate a method for predicting the downwash in a transverse plane behind a wing-body combination throughout an angle-of-attack range from 0 to 20 degrees. The predicted downwash was calculated by a numerical method in which an array of discrete vortices was allowed to roll up. The wing vortices were assumed to emanate from the trailing edge of the wing with their positions and strengths determined from the measured spanwise distribution of load.


Flight Stability and Automatic Control

Flight Stability and Automatic Control
Author: Robert C. Nelson
Publisher: WCB/McGraw-Hill
Total Pages: 441
Release: 1998
Genre: Aerodynamique / Aeronautique / Aerospatial / Automatique / Avion / Commande / Conception / Controle / Navigation / Stabilite
ISBN: 9780071158381

Download Flight Stability and Automatic Control Book in PDF, ePub and Kindle

The second edition of Flight Stability and Automatic Control presents an organized introduction to the useful and relevant topics necessary for a flight stability and controls course. Not only is this text presented at the appropriate mathematical level, it also features standard terminology and nomenclature, along with expanded coverage of classical control theory, autopilot designs, and modern control theory. Through the use of extensive examples, problems, and historical notes, author Robert Nelson develops a concise and vital text for aircraft flight stability and control or flight dynamics courses.


The Effective Downwash Characteristics at Transonic Speeds of a 6-percent-thick Wing with 47 Degrees of Sweepback in Combination with a Cylindrical Body as Determined from Force Measurements of a Horizontal Tail

The Effective Downwash Characteristics at Transonic Speeds of a 6-percent-thick Wing with 47 Degrees of Sweepback in Combination with a Cylindrical Body as Determined from Force Measurements of a Horizontal Tail
Author: Domenic A. Coppolino
Publisher:
Total Pages: 30
Release: 1952
Genre:
ISBN:

Download The Effective Downwash Characteristics at Transonic Speeds of a 6-percent-thick Wing with 47 Degrees of Sweepback in Combination with a Cylindrical Body as Determined from Force Measurements of a Horizontal Tail Book in PDF, ePub and Kindle


Investigation of the Downwash and Wake Behind a Triangular Wing of Aspect Ratio 4 at Subsonic and Supersonic Mach Numbers

Investigation of the Downwash and Wake Behind a Triangular Wing of Aspect Ratio 4 at Subsonic and Supersonic Mach Numbers
Author: Harold J. Walker
Publisher:
Total Pages: 32
Release: 1950
Genre: Airplanes
ISBN:

Download Investigation of the Downwash and Wake Behind a Triangular Wing of Aspect Ratio 4 at Subsonic and Supersonic Mach Numbers Book in PDF, ePub and Kindle

The effects of Mach number in the ranges between 0.50 and 0.95 and between 1.09 and 1.29 on the characteristics of the downwash and on the location of the wake behind a triangular wing of aspect ratio 4 have been determined from semispan model tests.


Experimental Wake Survey Behind a 120 Deg Included Angle Cone at Angles of Attack of 0 Deg and 5 Deg, Mach Numbers from 1.60 to 3.95, and Longitudinal Stations Varying from 1.0 to 8.39 Body Diameters

Experimental Wake Survey Behind a 120 Deg Included Angle Cone at Angles of Attack of 0 Deg and 5 Deg, Mach Numbers from 1.60 to 3.95, and Longitudinal Stations Varying from 1.0 to 8.39 Body Diameters
Author:
Publisher:
Total Pages: 356
Release: 1971
Genre:
ISBN:

Download Experimental Wake Survey Behind a 120 Deg Included Angle Cone at Angles of Attack of 0 Deg and 5 Deg, Mach Numbers from 1.60 to 3.95, and Longitudinal Stations Varying from 1.0 to 8.39 Body Diameters Book in PDF, ePub and Kindle