Atmosphere: Properties and Standard Atmosphere | Flight Mechanics | GATE Aero...Age of Aerospace
For Video Lecture of this presentation: https://youtu.be/DqaoNt0LoIE
The topics covered in this session are, Properties of Atmosphere, International Standard Atmosphere (ISA) definition and derivation, ISA Chart. The formula for obtaining ISA Chartar completely derived from basic equations.
Attention! "Gate Aerospace Engineering aspirants", A virtual guide for gate aerospace engineering is provided in "Age of Aerospace" blog for helping you meticulously prepare for gate examination. Respective notes of individual subjects are provided as 'Embedded Google Docs' which are frequently updated. This comprehensive guide is intended to efficiently serve as an extensive collection of online resources for "GATE Aerospace Engineering" which can be accessed free of cost. Use the following link to access the study material
https://ageofaerospace.blogspot.com/p/gate-aerospace.html
Atmosphere: Properties and Standard Atmosphere | Flight Mechanics | GATE Aero...Age of Aerospace
For Video Lecture of this presentation: https://youtu.be/DqaoNt0LoIE
The topics covered in this session are, Properties of Atmosphere, International Standard Atmosphere (ISA) definition and derivation, ISA Chart. The formula for obtaining ISA Chartar completely derived from basic equations.
Attention! "Gate Aerospace Engineering aspirants", A virtual guide for gate aerospace engineering is provided in "Age of Aerospace" blog for helping you meticulously prepare for gate examination. Respective notes of individual subjects are provided as 'Embedded Google Docs' which are frequently updated. This comprehensive guide is intended to efficiently serve as an extensive collection of online resources for "GATE Aerospace Engineering" which can be accessed free of cost. Use the following link to access the study material
https://ageofaerospace.blogspot.com/p/gate-aerospace.html
The term shock polar is generally used with the graphical representation of the Rankine-hugonoit eqution. This is either the hodograph plane or the pressure ratio-flow deflection angle plane .The polar itself is the locus of all possible states after an oblique shock.The minimum angle Ө, which an oblique shock can have is the mach no. µ=〖sin^(−1) (〗〖1/푀〗), where M is the initial mach no. before the shock and the shock greatest angle corresponds to a normal shock .
The range of shock angles is therefore sin^(−1)〖1/푀〗≤Ө≤Л/2
Pressure Altitude | Flight Mechanics | GATE AerospaceAge of Aerospace
For Video Lecture of this presentation: https://youtu.be/yO0IPxVZmwE
The topics covered in this session are pressure, density and temperature altitude. The practical significance of pressure altitude is discussed along with a real case example. An alternative method is also briefed
Attention! "Gate Aerospace Engineering aspirants", A virtual guide for gate aerospace engineering is provided in "Age of Aerospace" blog for helping you meticulously prepare for gate examination. Respective notes of individual subjects are provided as 'Embedded Google Docs' which are frequently updated. This comprehensive guide is intended to efficiently serve as an extensive collection of online resources for "GATE Aerospace Engineering" which can be accessed free of cost. Use the following link to access the study material
https://ageofaerospace.blogspot.com/p/gate-aerospace.html
This document explains briefly a Jet Fighter Aircraft Modeling Process in step by step bases. This model is made within SolidWorks.
A 1:1 Scale Dassault Mirage 2000 model.
Angle of attack | Flight Mechanics | GATE AerospaceAge of Aerospace
For Video Lecture of this presentation: https://youtu.be/GXKgH0guKqg
The topics covered in this session are, Definition: Angle of Attack (AOA), Insights,FoilSim AOA effect Visualization: Symmetric Airfoil, Cambered Airfoil, Flat Plate,Special Question: Why Airfoil?, Why not flat plate?
Attention! "Gate Aerospace Engineering aspirants", A virtual guide for gate aerospace engineering is provided in "Age of Aerospace" blog for helping you meticulously prepare for gate examination. Respective notes of individual subjects are provided as 'Embedded Google Docs' which are frequently updated. This comprehensive guide is intended to efficiently serve as an extensive collection of online resources for "GATE Aerospace Engineering" which can be accessed free of cost. Use the following link to access the study material
https://ageofaerospace.blogspot.com/p/gate-aerospace.html
The term shock polar is generally used with the graphical representation of the Rankine-hugonoit eqution. This is either the hodograph plane or the pressure ratio-flow deflection angle plane .The polar itself is the locus of all possible states after an oblique shock.The minimum angle Ө, which an oblique shock can have is the mach no. µ=〖sin^(−1) (〗〖1/푀〗), where M is the initial mach no. before the shock and the shock greatest angle corresponds to a normal shock .
The range of shock angles is therefore sin^(−1)〖1/푀〗≤Ө≤Л/2
Pressure Altitude | Flight Mechanics | GATE AerospaceAge of Aerospace
For Video Lecture of this presentation: https://youtu.be/yO0IPxVZmwE
The topics covered in this session are pressure, density and temperature altitude. The practical significance of pressure altitude is discussed along with a real case example. An alternative method is also briefed
Attention! "Gate Aerospace Engineering aspirants", A virtual guide for gate aerospace engineering is provided in "Age of Aerospace" blog for helping you meticulously prepare for gate examination. Respective notes of individual subjects are provided as 'Embedded Google Docs' which are frequently updated. This comprehensive guide is intended to efficiently serve as an extensive collection of online resources for "GATE Aerospace Engineering" which can be accessed free of cost. Use the following link to access the study material
https://ageofaerospace.blogspot.com/p/gate-aerospace.html
This document explains briefly a Jet Fighter Aircraft Modeling Process in step by step bases. This model is made within SolidWorks.
A 1:1 Scale Dassault Mirage 2000 model.
Angle of attack | Flight Mechanics | GATE AerospaceAge of Aerospace
For Video Lecture of this presentation: https://youtu.be/GXKgH0guKqg
The topics covered in this session are, Definition: Angle of Attack (AOA), Insights,FoilSim AOA effect Visualization: Symmetric Airfoil, Cambered Airfoil, Flat Plate,Special Question: Why Airfoil?, Why not flat plate?
Attention! "Gate Aerospace Engineering aspirants", A virtual guide for gate aerospace engineering is provided in "Age of Aerospace" blog for helping you meticulously prepare for gate examination. Respective notes of individual subjects are provided as 'Embedded Google Docs' which are frequently updated. This comprehensive guide is intended to efficiently serve as an extensive collection of online resources for "GATE Aerospace Engineering" which can be accessed free of cost. Use the following link to access the study material
https://ageofaerospace.blogspot.com/p/gate-aerospace.html
41. 長野滑空場
男体山
8150 ft
谷川岳
6441 ft
榛名山
4751 ft
松本
RJAF
相馬原
RJTU
宇都宮
RJTU
那須岳
6290 ft
安達太良山
5578 ft
板倉滑空場
赤城山
5998 ft
燧ケ岳
7697 ft
猪苗代湖
AREA 2
SFC-8000
尾瀬沼
中禅寺湖
G
G
福島
RJSF
①
板倉滑空場→日光
(男体山)→燧ケ岳
→榛名山→板倉
[高度約 7,000~
15,000ft]
②
板倉滑空場→日光
安達太良山→
東北方面→板倉
[高度約 8,000~
25,000ft]
③
長野滑空場→
谷川岳→日光→
東北方面
[高度約 8,000~
25,000ft]
グライダーによる高高度・長距離
クロスカントリー飛行の概略ルート (東北岩手山方面)
浅間山
8340 ft
高原山
5889 ft
自衛隊高高度訓練/試験空域
AREA H SFC- FL230
(AREA 3 の部分も含む)
月-土 0700‐2100 JST
OFF SIDE 124.9 133.9
YOKOTA APP 118.3(6000ft-FL175)
120.7(5500 ft↓)
自衛隊低高度訓練/試験空域
AREA 3 SFC-10000
DAILY 0700-2100 JST
OFF SIDE 124.9 133.9
412018/12/15