IN high‐speed level flight in the compressibility region an entirely new factor makes its appearance, viz: small variations of atmospheric density and speed of sound with height. This factor affects dynamic stability due to continuous changes of height during longitudinal disturbances; there is no effect in lateral disturbances. The affects are very small in low‐speed flight but they increase steadily with Mach number. The short‐period oscillations are not affected but the corrections to phugoid motion become appreciable in high subcritical flight, larger in supercritical (transonic) range, and very important in supersonic flight. The effects of compressibility are of paramount significance but they should be considered in conjunction with varying height effects. Another result of the investigation is the appearance of a new mode of disturbance, due to the stability quartic being converted into a quintic. The fifth (real) root is often small, it may vary in sign according to aerodynamic properties of the aircraft and characteristics of the power unit. The new mode is a subsidence or a divergence, and it determines height stability or instability, hence it may show to what extent an aircraft is able to keep constant altitude over long stretches of time.
Article navigation
Review Article|
November 01 1950
Longitudinal Stability, Speed and Height: An Examination of Dynamic Longitudinal Stability in Level Flight, Including the Effects of Compressibility and changes in Atmospheric Phenomena with Height
S. Neumark, Techn.Sc.D., A.F.R.Ae.S., A.F.I.Ae.S.
S. Neumark, Techn.Sc.D., A.F.R.Ae.S., A.F.I.Ae.S.
Search for other works by this author on:
Publisher: Emerald Publishing
Online ISSN: 2059-9366
Print ISSN: 0002-2667
© MCB UP Limited
1950
Aircraft Engineering (1950) 22 (11): 323–334.
Citation
Neumark S (1950), "Longitudinal Stability, Speed and Height: An Examination of Dynamic Longitudinal Stability in Level Flight, Including the Effects of Compressibility and changes in Atmospheric Phenomena with Height". Aircraft Engineering, Vol. 22 No. 11 pp. 323–334, doi: https://doi.org/10.1108/eb031964
Download citation file:
260
Views
Suggested Reading
UAV generalized longitudinal model for autopilot controller designs
Aircraft Engineering and Aerospace Technology: An International Journal (November,2021)
Autopilot design for an aircraft by using Luenberger observer design
Aircraft Engineering and Aerospace Technology: An International Journal (August,2018)
Application of virtual flight test framework with derivative design optimization
Aircraft Engineering and Aerospace Technology: An International Journal (November,2018)
A numerical study into the longitudinal dynamic stability of the tailless aircraft
Aircraft Engineering and Aerospace Technology: An International Journal (October,2018)
Re-modified quintic B-spline collocation method for the solution of Kuramoto–Sivashinsky type equations
Multidiscipline Modeling in Materials and Structures (November,2018)
Related Chapters
Working at heights
CDM 2015 Questions and Answers: A practical approach
The Conversion of Spectral Wave Heights to Design Wave Heights
Coasts, Marine Structures and Breakwaters 2017
9 Working at heights
Construction safety questions and answers: a practical approach
Recommended for you
These recommendations are informed by your reading behaviors and indicated interests.
