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The conceptual design of a Mach 2 Oblique Flying Wing supersonic transport

机译：mach 2斜飞翼超音速运输的概念设计

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This paper is based on a performance and economics study of a Mach two oblique flying wing transport aircraft that is to replace the B747B. In order to fairly compare our configuration with the B747B an equal structural technology level is assumed. It will be shown that the oblique flying wing configuration will equal or outperform the B747 in speed, economy and comfort while a modern stability and control system will balance the aircraft and smooth out gusts. The aircraft is designed to comply with the FAR25 airworthiness requirements and FAR36 stage 3 noise regulations. Geometry, aerodynamics, stability and control parameters of the oblique flying wing transport are discussed.

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Vandervelden, Alexander J. M.;
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年度 1989
页码 1-39
总页数 39
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AERODYNAMIC CONFIGURATIONS; AIRCRAFT CONFIGURATIONS; AIRCRAFT DESIGN; DESIGN ANALYSIS; FEASIBILITY ANALYSIS; OBLIQUE WINGS; SUPERSONIC TRANSPORTS; TAILLESS AIRCRAFT; AERODYNAMIC CHARACTERISTICS; AIRCRAFT CONTROL; AIRCRAFT PERFORMANCE; AIRCRAFT STABILITY; ECONOMIC FACTORS; OPTIMIZATION; STRUCTURAL DESIGN;

机译：空气动力学配置;飞机配置;飞机设计;设计分析;可行性分析; OBLIQUE WINGs;超级运输; TaILLEss aIRCRaFT;空气动力学特征;飞机控制;飞机性能;飞机稳定性;经济因素;优化;结构设计;

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专利

1. Manual Aerodynamic Optimization of an Oblique Wing Supersonic Transport [J] . Pei Li, Helmut Sobieczky, Richard Seebass Journal of Aircraft . 1999,第6期

机译：斜翼超音速运输的手动气动优化
2. Conceptual design analysis of a variable swept half-span wing of a supersonic business jet [J] . Alvaro Martins Abdalla, Felipe de Castro Baraky, Matheus Urzedo Quirino CEAS Aeronautical Journal . 2020,第4期

机译：超音速商务射流变量扫过半跨度翼的概念设计分析
3. Conceptual Design, Flying, and Handling Qualities Assessment of a Blended Wing Body (BWB) Aircraft by Using an Engineering Flight Simulator [J] . Clayton Humphreys-Jennings, Ilias Lappas, Dragos Mihai Sovar Aerospace . 2020,第5期

机译：使用工程飞行模拟器的混合翼体（BWB）飞机的概念设计，飞行和处理素质评估
4. Supersonic Bi- Directional Flying Wing, Part II: Conceptual Design of A High Speed Civil Transport [C] . D. Espinal, B. Lee, H. Sposato, AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition . 2010

机译：超音速双向飞行翼，第二部分：高速民用运输的概念设计
5. Integrated aerodynamic and control system design of oblique wing aircraft. [D] . Morris, Stephen James. 1990

机译：斜翼飞机的空气动力学和控制系统集成设计。
6. Aerodynamic evaluation of wing shape and wing orientation in four butterfly species using numerical simulations and a low-speed wind tunnel and its implications for the design of flying micro-robots [O] . Alejandro Ortega Ancel, Rodney Eastwood, Daniel Vogt, 2017

机译：利用数值模拟和低速风洞对四种蝶类的翼形和翼向进行空气动力学评估及其对飞行微型机器人设计的启示
7. On the oblique breakdown mechanism in a supersonic boundary layer on a swept wing at Mach 2 [O] . A. V. Panina, A. D. Kosinov, N. V. Semionov, 2017

机译：在马赫2的扫翼上的超声边界层中的倾斜击穿机制
8. Conceptual Design of a Mach 2 Oblique Flying Wing Supersonic Transport [R] . Vandervelden, A. J. M. 1989

机译：mach 2斜飞翼超音速运输的概念设计

The conceptual design of a Mach 2 Oblique Flying Wing supersonic transport

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