Results 301 to 310 of about 416,562 (354)
Some of the next articles are maybe not open access.
2019
The Concorde represented a highlight of the British-French aviation collaboration. This Mach 2+ aircraft required numerous compromises to produce a commercial aircraft with the ability to service intercontinental routes. The delta wing design provides optimal lift and drag during the high-speed cruise portion of flight.
openaire +1 more source
The Concorde represented a highlight of the British-French aviation collaboration. This Mach 2+ aircraft required numerous compromises to produce a commercial aircraft with the ability to service intercontinental routes. The delta wing design provides optimal lift and drag during the high-speed cruise portion of flight.
openaire +1 more source
Crashworthy Landing Gear Design
2017<div class="section abstract"> <div class="htmlview paragraph">The intent of this SAE Aerospace Information Report (AIR) is to document the design requirements and approaches for the crashworthy design of aircraft landing gear.</div> <div class="htmlview paragraph">This document covers the field of commercial and military ...
openaire +2 more sources
Landing Gear Ancillary Equipment
Aircraft Engineering and Aerospace Technology, 1968THE major problems concerning aircraft tyre design are the high ground speeds involved, very high braking torques which have to be transmitted, high temperatures which can be generated in the brakes and transferred to the tyres, as well as the stringent weight and space limitations imposed.
openaire +1 more source
Aircraft Engineering and Aerospace Technology, 1989
Aircraft undercarriage design involves the application and dissipation of energy within all the various mechanisms making up the complete gear. The functions of landing, taxying, retraction, lowering, steering and braking must be optimised such that each participating component plays its part in the processes.
openaire +1 more source
Aircraft undercarriage design involves the application and dissipation of energy within all the various mechanisms making up the complete gear. The functions of landing, taxying, retraction, lowering, steering and braking must be optimised such that each participating component plays its part in the processes.
openaire +1 more source
2017
<div class="section abstract"> <div class="htmlview paragraph">The purpose of this Aerospace Information Report is to provide the industry with methodologies for measuring tire/wheel gear alignment and the range of acceptable alignment settings for various types of non-military landing gear.
openaire +1 more source
<div class="section abstract"> <div class="htmlview paragraph">The purpose of this Aerospace Information Report is to provide the industry with methodologies for measuring tire/wheel gear alignment and the range of acceptable alignment settings for various types of non-military landing gear.
openaire +1 more source
<div class="section abstract"> <div class="htmlview paragraph">This SAE Aerospace Information Report (AIR) discusses the nature of landing gear stability, describes many common landing gear stability problems, and suggests approaches and methods for solving or avoiding them.</div></div>
openaire +1 more source
openaire +1 more source
Intelligent Service Robotics, 2022
Tsun-Cheng Huang, A. Elibol, N. Chong
semanticscholar +1 more source
Tsun-Cheng Huang, A. Elibol, N. Chong
semanticscholar +1 more source
2018
<div class="section abstract"> <div class="htmlview paragraph">The present document addresses gas and hydraulic fluid servicing required on commercial and military aircraft landing gears, for both single and dual chamber (also known as dual stage and two stage) shock struts.
openaire +1 more source
<div class="section abstract"> <div class="htmlview paragraph">The present document addresses gas and hydraulic fluid servicing required on commercial and military aircraft landing gears, for both single and dual chamber (also known as dual stage and two stage) shock struts.
openaire +1 more source
Crashworthy Landing Gear Study
1973Abstract : The purpose of the reported effort was twofold: to develop rotary- wing landing gear concepts and criteria which, when applied, would lessen the magnitude of crash forces transferred to occupiable areas of helicopters involved in severe yet survivable accidents; to use the concepts and criteria to design, fabricate, and test an experimental ...
Richard S. Scranton +2 more
openaire +1 more source
2019
<div class="section abstract"> <div class="htmlview paragraph">This document outlines the most common repairs used on landing gear components. It is not the intention of this AIR to replace overhaul/component maintenance or technical order manuals, but it can serve as a guide into their preparation.
openaire +1 more source
<div class="section abstract"> <div class="htmlview paragraph">This document outlines the most common repairs used on landing gear components. It is not the intention of this AIR to replace overhaul/component maintenance or technical order manuals, but it can serve as a guide into their preparation.
openaire +1 more source

