Aerodynamic, Stability and Flying Quality Evaluation on a Small Blended Wing-body Aircraft with Canard Foreplanes-Reference-Cited by-同舟云学术

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Aerodynamic, Stability and Flying Quality Evaluation on a Small Blended Wing-body Aircraft with Canard Foreplanes

Published:2014 Issue: Volume:15 Page:783-791
ISSN:2212-0173
Container-title:Procedia Technology
language:en
Short-container-title:Procedia Technology

Author:

Nasir Rizal E.M.,Kuntjoro Wahyu,Wisnoe Wirachman

Publisher

Elsevier BV

Subject

General Earth and Planetary Sciences,General Environmental Science

Reference19 articles.

1. The Horten Brothers and Their All-wing Aircraft;Myhra,1997

2. Jack Northrop and the Flying Wing: The Real Story Behind the Stealth Bomber;Coleman,1988

3. B-2 Spirit: The Most Capable War Machine on the Planet;Pace,1999

4. Blended Wing Body Subsonic Commercial Transport;Liebeck;AIAA Technical Paper 98-0438,1998

5. Stall resistance features of lifting body airplane configurations;Katz;Journal of aircraft,1999

Cited by 12 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Aerodynamic Evaluation of UiTM's Blended Wing Body Unmanned Aerial Vehicle at Different Elevon Configurations using Vortex Lattice Method;J AERONAUT ASTRONAUT;2024

2. Aerodynamic Investigation of Blended Wing Body Configuration;Defence Science Journal;2023-05-12

3. Structural Analysis of 3D Printed UAV Straight Wing Box;J AERONAUT ASTRONAUT;2022

4. Investigation on improving longitudinal static stability of a blended wing body aircraft;CEAS Aeronautical Journal;2021-08-13

5. Flight Dynamic Stability Performance of the Baseline-IX Blended-Wing-Body Unmanned Aerial System Using Flight Simulator;J AERONAUT ASTRONAUT;2021

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