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Aircraft Configurations Developing High Lift-drag Ratios at High Supersonic Speeds

1956 Aerodynamics
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Release : 1956
Genre : Aerodynamics
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Book Synopsis Aircraft Configurations Developing High Lift-drag Ratios at High Supersonic Speeds by : A. J. Eggers (Jr.)

Download or read book Aircraft Configurations Developing High Lift-drag Ratios at High Supersonic Speeds written by A. J. Eggers (Jr.). This book was released on 1956. Available in PDF, EPUB and Kindle. Book excerpt: Summary: The problem of designing an aircraft which will develop high lift-drag ratios in flight at high supersonic speeds is attacked using the elementary principle that the components of the aircraft should be individually and collectively arranged to impart the maximum downward and the minimum forward momentum to the surrounding air. This principle in conjunction with other practical considerations of hypersonic flight leads to the study of configurations for which the body is situated entirely below the wing; that is, flat-top wing-body combinations. Theory indicates that sensibly complete aircraft of this type can be designed to develop lift-drag ratios well in excess of 6.

Aircraft Configurations Developing High Lift-drag Ratios at High Supersonic Speeds

2023-07-18
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Release : 2023-07-18
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Book Rating : 656/5 ( reviews)

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Book Synopsis Aircraft Configurations Developing High Lift-drag Ratios at High Supersonic Speeds by : Ames Research Center

Download or read book Aircraft Configurations Developing High Lift-drag Ratios at High Supersonic Speeds written by Ames Research Center. This book was released on 2023-07-18. Available in PDF, EPUB and Kindle. Book excerpt: Aircraft Configurations is a comprehensive guide to the design and testing of supersonic aircraft. Based on research conducted at the Ames Research Center, it provides valuable insights into the aerodynamics of high-speed flight and the challenges of designing aircraft that can operate at these speeds. This book is an essential resource for anyone interested in the science of aviation. This work has been selected by scholars as being culturally important, and is part of the knowledge base of civilization as we know it. This work is in the "public domain in the United States of America, and possibly other nations. Within the United States, you may freely copy and distribute this work, as no entity (individual or corporate) has a copyright on the body of the work. Scholars believe, and we concur, that this work is important enough to be preserved, reproduced, and made generally available to the public. We appreciate your support of the preservation process, and thank you for being an important part of keeping this knowledge alive and relevant.

Aircraft Configurations Developed High Lift-drag Ratios at High Supersonic Speeds

1956
Download Aircraft Configurations Developed High Lift-drag Ratios at High Supersonic Speeds PDF Online Free

Author :
Release : 1956
Genre :
Kind : eBook
Book Rating : /5 ( reviews)

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Book Synopsis Aircraft Configurations Developed High Lift-drag Ratios at High Supersonic Speeds by : A.J. Jr Eggers

Download or read book Aircraft Configurations Developed High Lift-drag Ratios at High Supersonic Speeds written by A.J. Jr Eggers. This book was released on 1956. Available in PDF, EPUB and Kindle. Book excerpt:

A Supersonic Area Rule and an Application to the Design of a Wing-body Combination with High Lift-drag Ratios

1960 Airplanes
Download A Supersonic Area Rule and an Application to the Design of a Wing-body Combination with High Lift-drag Ratios PDF Online Free

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Release : 1960
Genre : Airplanes
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Book Synopsis A Supersonic Area Rule and an Application to the Design of a Wing-body Combination with High Lift-drag Ratios by : Richard T. Whitcomb

Download or read book A Supersonic Area Rule and an Application to the Design of a Wing-body Combination with High Lift-drag Ratios written by Richard T. Whitcomb. This book was released on 1960. Available in PDF, EPUB and Kindle. Book excerpt: Summary: As an extension of the transonic area rule, a concept for interrelating the wave drags of wing-body combinations at moderate supersonic speeds with axial developments of cross-sectional area has been derived. The wave drag of a combination at a given supersonic speed is related to a number of developments of cross-sectional areas as intersected by Mach planes. On the basis of this concept and other design procedures, a structurally feasible, swept-wing--indented-body combination has been designed to have relatively high maximum lift-drag ratios over a range of transonic and moderate supersonic Mach numbers. The wing of the combination has been designed to have reduced drag associated with lift and, when used with an indented body, to have low zero-lift wave drag. Experimental results have been obtained for this configuration at Mach numbers from 0.80 to 2.01. Maximum lift-drag ratios of approximately 14 and 9 were measured at Mach numbers of 1.15 and 1.41, respectively.

Factors Affecting the Maximum Lift-drag Ratio at High Supersonic Speeds

1956 Aerodynamics, Supersonic
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Release : 1956
Genre : Aerodynamics, Supersonic
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Book Synopsis Factors Affecting the Maximum Lift-drag Ratio at High Supersonic Speeds by : Charles H. McLellan

Download or read book Factors Affecting the Maximum Lift-drag Ratio at High Supersonic Speeds written by Charles H. McLellan. This book was released on 1956. Available in PDF, EPUB and Kindle. Book excerpt: A study of the factors affecting the maximum lift-drag ratio has been conducted in an effort to determine how to obtain high aerodynamic values at high supersonic Mach numbers.

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