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Title: AIRCRAFT STABILITY AND CONTROL
Page Link: AIRCRAFT STABILITY AND CONTROL -
Posted By: computer girl
Created at: Friday 08th of June 2012 03:32:08 PM
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AIRCRAFT STABILITY AND CONTROL



POWER EFFECT DUE TO JET PROPULSION

THERE ARE THREE MAJOR CONTRIBUTION
• DIRECT THRUST EFFECT
• DIRECT NORMAL FORCE EFFECT AT AIR DUCT
INTAKE
• INDUCED FLOW AT THE TAIL DUE TO THE
INFLOW TO THE JET BLAST
NOTE: THE ROCKET INSTALLATION WILL ENCOUNTER
FIRST TWO WHILE TURBOJET WILL ENCOUNTER ALL
THREE
....etc

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Title: The Full Flowpath Analysis of a Hypersonic Vehicle
Page Link: The Full Flowpath Analysis of a Hypersonic Vehicle -
Posted By: seminar class
Created at: Tuesday 03rd of May 2011 12:13:54 PM
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Abstract
A numerical study has been carried out to investigate the full flow path and aerodynamic characteristics of a hypersonic vehicle ata 7.0 free stream Mach number. Results indicate that the inlet started and unstarted operations have remarkable effects on the flow patternof the full flow path. When the inlet operates in a started mode, the transverse pressure gradient generated by the forebody alters theair captured characteristics and the entering flow quality of the inlet. Furthermore, the expansion proces ....etc

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Title: Evaluation of a Gamma Titanium Aluminide for Hypersonic Structural Applications
Page Link: Evaluation of a Gamma Titanium Aluminide for Hypersonic Structural Applications -
Posted By: Computer Science Clay
Created at: Sunday 07th of June 2009 12:22:57 PM
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Titanium matrix composites (TMCs) have been extensively evaluated for their potential to replace conventional superalloys in high temperature structural applications, as they provide significant weight-savings while maintaining comparable mechanical properties. Gamma titanium aluminide alloys and an appropriate fiber could offer an improved TMC for use in intermediate temperature applications (400-800°C). The purpose of this investigation is aimed at evaluating the potential of a gamma titanium aluminide alloy with nominal co ....etc

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Title: Morphing Aircraft Technology New Shapes For Aircraft Design
Page Link: Morphing Aircraft Technology New Shapes For Aircraft Design -
Posted By: thriveni898
Created at: Monday 13th of February 2012 11:52:04 AM
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Title: Aircraft control Using Software techniqus
Page Link: Aircraft control Using Software techniqus -
Posted By: mechanical engineering crazy
Created at: Wednesday 05th of August 2009 08:05:26 PM
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Aircraft or airbus is controled with network i.e using software techq. All parts of aironautical Engg.is controlled by Using software or programming as well as all important task of airbus is control by software it means there is no need to pilot to drive the airbus,it is totally based on software. ....etc

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Title: hypersonic sound system full report
Page Link: hypersonic sound system full report -
Posted By: project reporter
Created at: Monday 01st of February 2010 03:05:56 PM
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ABSTRACT
Hypersonic sound technology from American Technology Corporation employs ultrasonic waves to create audible sound in the air. It works by using harmless ultrasonic tones that we can't hear. These tones use the property of air to create new tones that are within the range of human hearing. The result is audible sound. The acoustical sound wave is created directly in the air molecules by down-converting ultrasonic energy to the frequency spectrum we can hear. Hyper Sonic Sound is produced without the excess bag ....etc

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Title: Morphing Aircraft Technology New Shapes For Aircraft Design
Page Link: Morphing Aircraft Technology New Shapes For Aircraft Design -
Posted By: seminar project explorer
Created at: Tuesday 15th of March 2011 11:39:28 PM
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Morphing Aircraft Technology
&
New Shapes For Aircraft Design
V.Vikram
S6 Department of Mechanical Engineering
Mohandas college of Engineering and Technology



Abstract
Morphing aircraft are multi-role aircraft that change their external shape substantially to adapt to a changing
mission environment during flight.2 This creates superior system capabilities not possible without morphing shape
changes. The objective of morphing activities is to develop hig ....etc

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Title: free ppt for a hypersonic hybrid vehicle
Page Link: free ppt for a hypersonic hybrid vehicle -
Posted By:
Created at: Tuesday 16th of October 2012 05:30:05 AM
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Title: aircraft control cable lubrication
Page Link: aircraft control cable lubrication -
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Created at: Friday 19th of September 2014 01:10:15 AM
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Title: aircraft autopilot roll control system pdf
Page Link: aircraft autopilot roll control system pdf -
Posted By:
Created at: Sunday 22nd of March 2015 10:48:51 PM
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