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Flight test evaluation and analysis ...
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Hays, Mitchell J.
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Flight test evaluation and analysis of the l-39C Albartros for the light attack mission.
紀錄類型:
書目-電子資源 : Monograph/item
正題名/作者:
Flight test evaluation and analysis of the l-39C Albartros for the light attack mission./
作者:
Hays, Mitchell J.
面頁冊數:
173 p.
附註:
Source: Masters Abstracts International, Volume: 55-01.
Contained By:
Masters Abstracts International55-01(E).
標題:
Aerospace engineering. -
電子資源:
http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=1595496
ISBN:
9781321947908
Flight test evaluation and analysis of the l-39C Albartros for the light attack mission.
Hays, Mitchell J.
Flight test evaluation and analysis of the l-39C Albartros for the light attack mission.
- 173 p.
Source: Masters Abstracts International, Volume: 55-01.
Thesis (M.S.)--Saint Louis University, 2015.
Aircraft test and evaluation is a key component of aircraft development and design verification. Developmental flight test, an early look into aircraft functionality and mission suitability, is conducted early in the aircraft lifecycle to mitigate cost, schedule, and performance risks. This thesis details the ground and flight test of the L-39C "Albatros" for the light attack mission.
ISBN: 9781321947908Subjects--Topical Terms:
1002622
Aerospace engineering.
Flight test evaluation and analysis of the l-39C Albartros for the light attack mission.
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173 p.
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Source: Masters Abstracts International, Volume: 55-01.
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Adviser: Lawrence Boyer.
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Thesis (M.S.)--Saint Louis University, 2015.
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Aircraft test and evaluation is a key component of aircraft development and design verification. Developmental flight test, an early look into aircraft functionality and mission suitability, is conducted early in the aircraft lifecycle to mitigate cost, schedule, and performance risks. This thesis details the ground and flight test of the L-39C "Albatros" for the light attack mission.
520
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The L-39C was evaluated as a light attack aircraft to determine aircraft performance, handling qualities, and human-machine interface to support specification validation and document mission utility. The specifications and scenario were generated by instructors at the United States Naval Test Pilot School (USNTPS) as part of the Engineering Test Pilot curriculum. Classical flight test techniques were used to elicit open loop aircraft response and performance characterization. Additionally, various mission representative maneuvers were executed to aid in identification of deficiencies in aircraft handling qualities.
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This work is adapted from the author's work at the USNTPS and presents data associated with the capstone exercise of the USNTPS Experimental Test Pilot syllabus.
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The results of this thesis clearly illustrate the suitability of the L-39C for the light attack mission.
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