Aerodynamic Properties Of Cruciform Wing And Body Combinations At Subsonic Transonic And Supersonic Speeds PDF Download

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Aerodynamic Properties of Cruciform-wing and Body Combinations at Subsonic, Transonic, and Supersonic Speeds

Aerodynamic Properties of Cruciform-wing and Body Combinations at Subsonic, Transonic, and Supersonic Speeds
Author: John R. Spreiter
Publisher:
Total Pages: 646
Release: 1949
Genre: Aerodynamic load
ISBN:

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The aerodynamic forces and moments exerted on pitched and yawed wing-body combinations consisting of a slender body of revolution and a cruciform arrangement of thin wings have been investigated by two theoretical methods. One method, an extension of the slender wing-body theory of NACA TN No. 1662, makes possible the determination of simple closed expressions for the load distribution, of simple closed expressions for the load distribution, the forces, and the moments for slender cruciform-wing and body combinations in which the wings may be dissimilar plan form. The second method treats cruciform-wing and body combinations consisting of a body of revolution and identical wings of arbitrary aspect ratio and plan form. The results are valid at subsonic, transonic, and supersonic speeds.


Aerodynamic Properties of Slender Wing-body Combinations at Subsonic, Transonic, and Supersonic Speeds

Aerodynamic Properties of Slender Wing-body Combinations at Subsonic, Transonic, and Supersonic Speeds
Author: John R. Spreiter
Publisher:
Total Pages: 33
Release: 1948
Genre: Aerodynamics
ISBN:

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It is further shown that the aerodynamic characteristics of a moderate-aspect-ratio pointed wing at sonic speed may be predictied in a manner mathematically equivalent to that used in the study of a low-aspect-ratio wing.


Annual Report - National Advisory Committee for Aeronautics

Annual Report - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Total Pages:
Release: 1957
Genre: Aeronautics
ISBN:

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Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.


Report

Report
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Total Pages: 18
Release: 1957
Genre: Aeronautics
ISBN:

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Aerodynamic Investigation at Mach Number 1.92 of a Rectangular Wing and Tail and Body Configuration and Its Components

Aerodynamic Investigation at Mach Number 1.92 of a Rectangular Wing and Tail and Body Configuration and Its Components
Author: Macon C. Ellis
Publisher:
Total Pages: 104
Release: 1950
Genre: Airplanes
ISBN:

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An investigation at Mach number 1.92 in the Langley 9-inch supersonic tunnel of a variable body-wing-tail configuration has been made in order to determine and to isolate the aerodynamic effects on each other of the components of the configuration.


Aerodynamics

Aerodynamics
Author: Mofid Gorji-Bandpy
Publisher: BoD – Books on Demand
Total Pages: 250
Release: 2021-02-10
Genre: Science
ISBN: 1838801677

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Aerodynamics, the study of air motion around solid objects, allows us to understand and measure the dominating forces acting on aircrafts, buildings, bridges, automobiles, and other structures. The forces that result in an aircraft overcoming gravity and drag are called thrust and lift. Various parameters such as geometrical configurations of objects, as well as physical properties of air, which may be functions of position and time, affect those forces. This book covers some of the latest studies regarding the application of the principles of aerodynamics to the design of many different engineered objects. This book will be of interest to mechanical and aerospace engineering students, academics, and researchers who are looking for new insights into this fascinating branch of fluid mechanics.