Filters
Indirect omega-k scheme of the lift surface flutter calculation with controls in MATHCAD
Limited calculation of aerodynamic damping and frequencies versus an indirect counted flight speed of a lift surface with controls on a base of 2D Theodorsen´s non-stationary profile theory for the input of mass characteris...
JU - Aeronautika, aerodynamika, letadla
- 2007 •
- X
Rok uplatnění
X - Nezařazeno
Flutter Calculation Model with Isolated Modal Characteristics of Control Surfaces for Small Sport Airplanes
Lagrange´s model of flutter equation of a lift surface with two control surfaces based on modal characteristics of the lift surface with fixed control surfaces and isola...
JU - Aeronautika, aerodynamika, letadla
- 2008 •
- Jx
Rok uplatnění
Jx - Nezařazeno - Článek v odborném periodiku (Jimp, Jsc a Jost)
Direct p-k scheme of wing and empennage flutter characteristics with control surfaces of small sport aircraft.
of wings and empennages with control surfaces for a given flight speed and altitude of aharmonically oscillated thin profile with control surface and 3D corrections for plans of lift surfaces. In...
JU - Aeronautika, aerodynamika, letadla
- 2010 •
- R
Rok uplatnění
R - Software
Modal Methodical tests of the Wing and Empennage with Control Surfaces of VL-3 Aircraft for Acquisition of Mass-Stiffness Characteristics
to a lift surface and individual control surfaces needed for a computational flutter analysis of the lift surface with control surfaces.Systematic ground frequency test...
JU - Aeronautika, aerodynamika, letadla
- 2007 •
- O
Rok uplatnění
O - Ostatní výsledky
DESIGN FOR ACTIVE FLUTTER SUPPRESION AND MODEL VERIFICATION
lifting surface with control surface controlled by pilot and supplementary control flutter suppression on an aircraft structure. The supplementary control surface is pl...
JU - Aeronautika, aerodynamika, letadla
- 2016 •
- Jx •
- Link
Rok uplatnění
Jx - Nezařazeno - Článek v odborném periodiku (Jimp, Jsc a Jost)
Výsledek na webu
DESIGN FOR ACTIVE FLUTTER SUPPRESION AND MODEL VERIFICATION
lifting surface with control surface controlled by pilot and supplementary control flutter suppression on an aircraft structure. The supplementary control surface is pl...
JU - Aeronautika, aerodynamika, letadla
- 2016 •
- D •
- Link
Rok uplatnění
D - Stať ve sborníku
Výsledek na webu
FLUTTER ANALYSIS OF THE PHOENIX AIRPLANE
characteristic for lifting surfaces and control surfaces of the airplane is included in the report. In addition, the flutter analysis based on those data is carried out by p-k methods. The influence of
Aerospace engineering
- 2023 •
- O
Rok uplatnění
O - Ostatní výsledky
FLUTTER ANALYSIS OF THE AIRPLANE HARMONY
characteristic for lifting surfaces and control surfaces of the airplane is included in the report. In addition, the flutter analysis based on those data is carried out by p-k methods. The influence of to...
Aerospace engineering
- 2022 •
- O
Rok uplatnění
O - Ostatní výsledky
Trial Calculations of Aerodynamic Damping and Frequencies of the Wing and Empennage with Controls Surfaces of VL-3 Aircraft by Means of the Indirect "omega-k" Computation Model
characteristics distribution along lift and control surfaces. Flight speed is captured of individual degrees of freedom of wing with ailerons and empennage with controls surfaces evaluated from ground fre...
JU - Aeronautika, aerodynamika, letadla
- 2007 •
- O
Rok uplatnění
O - Ostatní výsledky
Unsteady Aerodynamic Forces Measured on a Fluttering Profile
near the fluttering profile NACA0015 with two-degrees of freedom, Mach number of the flutter occurrence were M=0.21 and M=0.45. Aerodynamic forces (drag and lift components) wereevaluated independently on the upper and low...
BI - Akustika a kmity
- 2014 •
- D •
- Link
Rok uplatnění
D - Stať ve sborníku
Výsledek na webu
- 1 - 10 out of 153 147