Constant altitude helicopter flight testing
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Authors
Layton, Donald M.
Safe, Per
Subjects
Advisors
Date of Issue
1986
Date
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Language
Abstract
Normalized W/a performance data for a helicopter can be obtained during a constant altitude flight with the same accuracy as the ratio can be obtained during a variable density flight. The only bound on this method is that the data acquisition be as rapid as possible to minimize the weight change during the data acquisition phase.
Type
Conference Paper
Description
AIAA/AHS/CASI/DGLR/IES/ISA/lTEA/SETP/SFTE 3rd Flight Testing Conference, April 2-4, 1986/Las Vegas, Nevada
Series/Report No
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NPS Report Number
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Funder
Format
6 p.
Citation
Layton, D. and Per Safe. "Constant altitude helicopter flight testing." 3rd Flight Testing Conference and Technical Display. 1986.
Distribution Statement
Rights
This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.