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Chapter 13 - PerformanceThis Section will set forth the types of tests, procedures, instrumentation requirements, data analysis and presentation, and the purposes for conducting performance tests. In general, performance tests are conducted to: 1) Determine those elements of the aircraft's performance which are critical from flight safety considerations, i.e., the weight/altitude/temperature limits at which the applicable performance requirements with respect to the take-off and landing distances and climb gradients are met; 2) Acquire data to quantify the capabilities of an aircraft, to verify and/or establish the aircraft's performance model, and to provide information for the Aircraft Operation Manual (AOM); and 3) Determine if an aircraft meets specifications/guarantees. There are a number of sources of detailed information on conducting performance tests, and analyzing and presenting data. A few of these sources are listed as references and a selected few are contained as bibliographic entries. [13-1, 13-2, 13-3] This Section offers a broad introduction to the topic: although based principally on typical civil practice, a similar approach is applied to military aircraft, and aspects specific to military aircraft, such as combat, are covered.
Document ID
20050209997
Acquisition Source
Legacy CDMS
Document Type
Other - Technical Report
Authors
J P K Vleghert
Date Acquired
August 23, 2013
Publication Date
July 1, 2005
Publication Information
Publication: Introduction to Flight Test Engineering [Introduction Aux Techniques Des Essais En Vol]
Publisher: North Atlantic Treaty Organization
Volume: 14
ISBN: 9283711262
Subject Category
Aircraft Design, Testing and Performance
Report/Patent Number
RTO-AG-300-V14
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
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