Analysis of spacecraft vehicle responses to atmospheric wind gusts during flight is important in the establishment of vehicle design structural requirement
This paper will analyze the Gust Load Alleviation (GLA) systems which can be used to reduce the effe...
The paper presents a methodology for calculating the flight dynamic characteristics and gust respons...
Fundamental phase in the preliminary design of an aircraft is the load case choice. Historically, th...
15th MST Radar WorkshopSession M4: MST Radar scattering, turbulence and small-scale processesMay 30 ...
A methodology for aeroelastic gust response of launch vehicles in flight is developed by using a pre...
The small scale of micro aerial vehicles (MAVs) provide the somewhat unique capability of full scale...
The stresses resulting from wind gusts can exceed the limit value and may cause large-scale structur...
ABSTRACT: Aerospace engineering has always had the need for various natural environment parameters t...
Abstract: The paper investigates the gusts action at the vertical maneuver phase (“Pitchov...
Four models are examined which attempt to describe wind fluctuations in relation to a wind energy co...
ABSTRACT Since atmospheric winds play the most critical natural enviroment (NE) role as input into t...
This project presents work performed by the Institute of Aerospace Engineering, Brno University of T...
Crosswind gusts have a continuous influence on the ride and handling of road vehicles. At low speeds...
A small unmanned aerial vehicle (SUAV) was developed with the specific objective to explore atmosphe...
th scale, aeroelastically equivalent Remotely Piloted Vehicle (RPV) is desired to investigate the gu...
This paper will analyze the Gust Load Alleviation (GLA) systems which can be used to reduce the effe...
The paper presents a methodology for calculating the flight dynamic characteristics and gust respons...
Fundamental phase in the preliminary design of an aircraft is the load case choice. Historically, th...
15th MST Radar WorkshopSession M4: MST Radar scattering, turbulence and small-scale processesMay 30 ...
A methodology for aeroelastic gust response of launch vehicles in flight is developed by using a pre...
The small scale of micro aerial vehicles (MAVs) provide the somewhat unique capability of full scale...
The stresses resulting from wind gusts can exceed the limit value and may cause large-scale structur...
ABSTRACT: Aerospace engineering has always had the need for various natural environment parameters t...
Abstract: The paper investigates the gusts action at the vertical maneuver phase (“Pitchov...
Four models are examined which attempt to describe wind fluctuations in relation to a wind energy co...
ABSTRACT Since atmospheric winds play the most critical natural enviroment (NE) role as input into t...
This project presents work performed by the Institute of Aerospace Engineering, Brno University of T...
Crosswind gusts have a continuous influence on the ride and handling of road vehicles. At low speeds...
A small unmanned aerial vehicle (SUAV) was developed with the specific objective to explore atmosphe...
th scale, aeroelastically equivalent Remotely Piloted Vehicle (RPV) is desired to investigate the gu...
This paper will analyze the Gust Load Alleviation (GLA) systems which can be used to reduce the effe...
The paper presents a methodology for calculating the flight dynamic characteristics and gust respons...
Fundamental phase in the preliminary design of an aircraft is the load case choice. Historically, th...