Hostname: page-component-cd9895bd7-p9bg8 Total loading time: 0 Render date: 2024-12-28T05:33:36.147Z Has data issue: false hasContentIssue false
  • English
  • Français

Relationships between flying qualities and flight tests parameters for the F/A-18 aircraft

Published online by Cambridge University Press:  03 February 2016

R. M. Botez  and
M. Rotaru
R. M. Botez
Affiliation:
Ecole de technologie supérieure, Laboratory of Research in Active Controls, Avionics and Aeroservoelasticity, Montréal, Canada
M. Rotaru
Affiliation:
Ecole de technologie supérieure, Laboratory of Research in Active Controls, Avionics and Aeroservoelasticity, Montréal, Canada
Get access Rights & Permissions [Opens in a new window]

Extract

In this Technical Note, is shown that relationships exist between flying qualities levels 1, 2 and 3 and flight conditions expressed in terms of Mach numbers, altitudes and angles-of-attack for the F/A-18 SRA (System Research Aircraft). These relationships are helpful in detecting if derivatives are well calculated for flight tests intermediate conditions.

Type
Technical Note
Information
The Aeronautical Journal , Volume 111 , Issue 1118 , April 2007 , pp. 281 - 282
Copyright
Copyright © Royal Aeronautical Society 2007 

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

1. Nelson, R.C., Flight Stability and Automatic Control, 1998, McGraw Hill, New York.Google Scholar