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Journal ArticleDOI

Unrestrained Aeroelastic Divergence in a Dynamic Stability Analysis

William P. Rodden, +1 more
- 01 Sep 1982 - 
- Vol. 19, Iss: 9, pp 796-797
TLDR
In this article, the authors compared the predicted counts of scheduled and unscheduled aircraft with the recorded counts for the above data for the times, 8 a.m.-6 p.m., on the hour.
Abstract
Comparison of Model Predictions with Field Data On July 13 (Friday), 1979, Cleveland center recorded the number of actively controlled aircraft as a function of time of day. (This recording also included a small number of controlled non-IFR aircraft.) Cleveland center, which controls the airspace over parts of Ohio, Michigan, New York, Pennsylvania, and West Virginia, is one of the busiest centers. The sum of the models' predicted counts of scheduled and unscheduled aircraft was compared with the recorded counts for the above data for the times, 8 a.m.-6 p.m., on the hour. At the time the comparisons were made, unscheduled aircounts could be predicted for any day in April 1978. Therefore seasonal adjustment factors for GA activity based on historical data were applied to these counts, so that they would be representative of counts on a typical Friday in July 1979. Figure 1 shows predicted IFR counts and actual counts over Cleveland center. (Data points are connected by lines as a visual aid.) Similar comparisons were made for Houston, Kansas City, and New York centers (one day for each center in the summer of 1979, although the day of the week was different in each case). All comparisons between predicted and measured aircounts show good agreement in terms of small numerical differences in the amplitudes and also similar harmonic content. The largest difference occurs at the peaks and is about 10%. This agreement is sufficient for system planning purposes. It is planned to extend these comparisons to other centers for additional days and seasons of the year, and to quantify the (statistical) differences between measured and predicted counts.

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Citations
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Journal ArticleDOI

Damping Perturbation Method for Flutter Solution: The g-Method

P. C. Chen
- 01 Jan 2000 - 
TL;DR: The g-method as mentioned in this paper generalizes the K-method and the P-K method for reliable damping prediction and utilizes a reduced-frequency sweep technique to search for the roots of the utter solution and a predictorcorrector scheme to ensure the robustness of the sweep technique.
Journal ArticleDOI

On the static aeroelastic tailoring of composite aircraft swept wings modelled as thin-walled beam structures☆

TL;DR: In this article, a thin-walled anisotropic composite beam model is adopted to analyze the static aeroelastic response and divergence instability of swept-forward aircraft wing structures constructed of anisotropy composite materials.
Journal ArticleDOI

Analytical Studies on Static Aeroelastic Behavior of Forward-Swept Composite Wing Structures

TL;DR: An exact methodology allowing one to determine the aeroelastic lift distribution and the divergence instability of swept cantilevered composite wing structures is developed in this paper.
Journal ArticleDOI

Aeroelastic stability characteristics of a composite swept wing withtip weights for an unrestrained vehicle

TL;DR: In this article, an analytical investigation to determine aeroelastic flutter and divergence behavior of a composite, forwardswept rectangular wing was conducted, where the wing was assumed to carry a fuselage at its semispan, a pylon at the wing tip, and the aircraft was in a free-flight condition (unrestrained vehicle).
Book

Flutter and Divergence Analysis using the Generalized Aeroelastic Analysis Method

TL;DR: The generalized aeroelastic analysis method solution procedure allows complete control over Mach number, velocity, density, andcomplexfrequency without recourse to complex mode tracking logic or dataset interpolation, as in the k, p–k, and g-solution methods.
References
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Book

Principles of aeroelasticity

TL;DR: In this article, aeroelasticite was used to construct an instationnaire for the structure reference record created on 2005-11-18, modified on 2016-08-08.
Journal ArticleDOI

A strip method for prediction of damping in subsonic wind tunnel andflight flutter tests.

TL;DR: In this article, a strip method has been developed for the prediction of subcritical damping characteristics for guidance of subsonic wind tunnel and flight flutter tests, where transient aerodynamic coefficients are found from a Fourier transform of the two-dimensional incompressible oscillatory coefficients.
Journal ArticleDOI

Aeroelastic divergence of unrestrained vehicles

TL;DR: In this paper, the effect of inertial relief on the aeroelastic redistribution of wing lift is discussed and a distinction is made between static divergence of a restrained vehicle and dynamic divergence of an unrestrained vehicle.