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Fundamental Assessment of High-Speed Aircraft Stability and Control from Historic Flight Tests.
紀錄類型:
書目-語言資料,手稿 : Monograph/item
正題名/作者:
Fundamental Assessment of High-Speed Aircraft Stability and Control from Historic Flight Tests./
作者:
Lorenzo, William P.
面頁冊數:
1 online resource (154 pages)
附註:
Source: Masters Abstracts International, Volume: 85-06.
Contained By:
Masters Abstracts International85-06.
標題:
Engineering. -
電子資源:
click for full text (PQDT)
ISBN:
9798381158885
Fundamental Assessment of High-Speed Aircraft Stability and Control from Historic Flight Tests.
Lorenzo, William P.
Fundamental Assessment of High-Speed Aircraft Stability and Control from Historic Flight Tests.
- 1 online resource (154 pages)
Source: Masters Abstracts International, Volume: 85-06.
Thesis (M.S.)--Arizona State University, 2023.
Includes bibliographical references
This work uses Arizona State University's (ASU) newly developed high-speed vehicle stability and control screening methodologies to reverse-engineer famous United States Air Force (USAF) flight tests from the 1950s and 1960s. This thesis analyzes the root cause of Chuck Yeager's fateful 1953 supersonic spin in the Bell X-1A to become the "Fastest Man Alive". This thesis then takes a look back at Neil Armstrong's inadvertent atmospheric skip in the North American X-15 and his subsequent hypersonic flight months later. The fundamental flying qualities assessment shown in this work begins with calculating rigid-body frequencies and damping ratios of an aircraft to Military Standard (MIL) requirements, and uses these to create a full, classical stability and control analysis of a high-speed vehicle. Through reverse engineering the flight envelopes and missions for the above aircraft, it appears that the near-disasters of each flight were due to a confluence of then overlooked, yet fundamental, aerodynamic instabilities.
Electronic reproduction.
Ann Arbor, Mich. :
ProQuest,
2024
Mode of access: World Wide Web
ISBN: 9798381158885Subjects--Topical Terms:
561152
Engineering.
Subjects--Index Terms:
Chuck YeagerIndex Terms--Genre/Form:
554714
Electronic books.
Fundamental Assessment of High-Speed Aircraft Stability and Control from Historic Flight Tests.
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Fundamental Assessment of High-Speed Aircraft Stability and Control from Historic Flight Tests.
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Source: Masters Abstracts International, Volume: 85-06.
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Advisor: Takahashi, Timothy.
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Thesis (M.S.)--Arizona State University, 2023.
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Includes bibliographical references
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This work uses Arizona State University's (ASU) newly developed high-speed vehicle stability and control screening methodologies to reverse-engineer famous United States Air Force (USAF) flight tests from the 1950s and 1960s. This thesis analyzes the root cause of Chuck Yeager's fateful 1953 supersonic spin in the Bell X-1A to become the "Fastest Man Alive". This thesis then takes a look back at Neil Armstrong's inadvertent atmospheric skip in the North American X-15 and his subsequent hypersonic flight months later. The fundamental flying qualities assessment shown in this work begins with calculating rigid-body frequencies and damping ratios of an aircraft to Military Standard (MIL) requirements, and uses these to create a full, classical stability and control analysis of a high-speed vehicle. Through reverse engineering the flight envelopes and missions for the above aircraft, it appears that the near-disasters of each flight were due to a confluence of then overlooked, yet fundamental, aerodynamic instabilities.
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click for full text (PQDT)
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