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AE-705 Introduction to Flight Lecture 01 Capsule-01 AE-705: Introduction to Flight STANDARD ATMOSPHERE Udit Vohra Aerospace Engineering Department PEC University of Technology, Chandigarh

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AE-705 Introduction to Flight Lecture 01 Capsule-01

AE-705: Introduction to Flight

STANDARD ATMOSPHERE

Udit Vohra Aerospace Engineering Department

PEC University of Technology, Chandigarh

AE-705 Introduction to Flight Lecture 01 Capsule-01

LAYOUT

• Earth’s Atmosphere

• Atmospheric Standards

• Different Altitudes

• Two magical equations

• Q Codes for altitudes

• Weather Effects

http://www.newtonsapple.org.uk/earth-as-a-magnet/

AE-705 Introduction to Flight Lecture 01 Capsule-01

ATMOSPHERE

http://www.slideshare.net/shalinipandey77985/res525-origin-of-earth-and -earth-atmosphere

AE-705 Introduction to Flight Lecture 01 Capsule-01

AEROSPACE VEHICLES

http://static1.businessinsider.com/image/5374f0df

6bb3f73f5c360e25-1200-

1715/ap090416034735.jpg https://iasmania.com/launch-vehicles-for-satellites-space-probes/

Atmospheric vehicles Space vehicles

Why do we need

to study these ?

To study the

design and

performance of

these vehicle

Lets see what I

got for you

Vehicles which fly

in earth’s

atmosphere only

Vehicles which

fly in deep space

eg -satellites

AE-705 Introduction to Flight Lecture 01 Capsule-01

ISA (International Standard Atmosphere)

Aerospace Vehicles Design and Performance determination

Simulation and Analysis

To relate

to a common reference

Properties of real atmosphere Constant

Why do we need ISA ?

Flight test Wind tunnel results A/C design and performance

Create a hypothetical model

ISA

AE-705 Introduction to Flight Lecture 01 Capsule-01

DIFFERENT ALTITUDES

What are they ?

Somebody

help..!!

AE-705 Introduction to Flight Lecture 01 Capsule-01

Geometric

Absolute

Geopotential Pressure Alt.

Temperature.

Alt.

Density Alt.

Somebody

help..!!

AE-705 Introduction to Flight Lecture 01 Capsule-01

Geometric

Absolute

Geopotential Pressure Alt.

Temperature.

Alt.

Density Alt.

Depends on whom

you ask..!!

We will study first

three for now These will be

studied later

AE-705 Introduction to Flight Lecture 01 Capsule-01

http://www.boldmethod.com/blog/lists/2017/05/the-5-types-of-flying-altitudes/

Indicated Altitude

AE-705 Introduction to Flight Lecture 01 Capsule-01

Geometric Altitude/True Altitude – altitude from sea level

http://www.boldmethod.com/blog/lists/2017/05/the-5-types-of-flying-altitudes/

Also called

GEOMETRIC ALTITUDE

AE-705 Introduction to Flight Lecture 01 Capsule-01

Absolute Altitude – Altitude from the center of earth

Anderson-Introduction%20to%20Flight-McGraw-Hill%20Science_Engineering_Math%20(2011).pdf

AE-705 Introduction to Flight Lecture 01 Capsule-01

Geopotential Altitude - variation in g is considered with the altitude

h =

Where h is the Geopotential altitude http://hemantmore.org/physics-1/p11202005/3898/

Geopotential altitude

is considered ONLY in

case of space vehicles Why not for atmospheric

vehicles??

Figure out yourself

&

report on Moodle..!!

AE-705 Introduction to Flight Lecture 01 Capsule-01

Hydrostatic Equation

https://wikis.engrade.com/energyandearthsatmospher

John%20Anderson-Introduction%20to%20Flight-

McGrawHill%20Science_Engineering_Math%20(2011).pdf

Fluid element at rest

AE-705 Introduction to Flight Lecture 01 Capsule-01

PARAMETER VARIATION WITH ALTITUDE

Pressure, temperature, density, viscosity

AE-705 Introduction to Flight Lecture 01 Capsule-01

Variation of

P and T

with

geometric

Altitude h

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Lets see it layer by layer

AE-705 Introduction to Flight Lecture 01 Capsule-01

Atmospheric vehicles (fly at

about 10km ) …so we will not

consider this part

Temperature Variation with Altitude

Gradient layer

Isothermal layer

Gradient layer

JohnAnderson-Introduction%20to%20Flight-McGraw-

Hill%20Science_Engineering_Math%20(2011).pdf

AE-705 Introduction to Flight Lecture 01 Capsule-01

P & ρ variation with altitude

Two magical equations

dp= - ρgdh

p= ρRT

Gradient layer

Isothermal

AE-705 Introduction to Flight Lecture 01 Capsule-01

Sutherland’s Formula

Viscosity

https://www.google.com/search?q=sutherland+formula+for+viscosity&source=lnms&tbm=isch&sa=X&sqi=2&ved=0ahUKEwjQ8OWao5TU

AhUDq48KHb_XC9kQ_AUIBigB&biw=1408&bih=671&dpr=0.97#imgrc=Lyv9kfZ5j2KqoM:&spf=1496032614588

AE-705 Introduction to Flight Lecture 01 Capsule-01

Pressure Altitude Altitude corresponding to the pressure values in the ISA table

Here –

the theoretical

location where at 15

degrees Celsius the

altimeter setting will

equal 29.92 inches

of mercury

Temp &

pressure

corrections

http://www.boldmethod.com/blog/lists/2017/05/the-5-types-of-flying-altitudes/

AE-705 Introduction to Flight Lecture 01 Capsule-01

Pressure altitude corrected for non-standard temperature

Density Altitude

htt

ps:

//w

ww

.m0

a.co

m/c

alcu

lati

ng

-den

sity

-alt

itude/

How to read

this graph ??

AE-705 Introduction to Flight Lecture 01 Capsule-01

Altitude corresponding to the temp values in the ISA table

Temperature Altitude

https://www.aopa.org/news-and-media/all-news/2015/april/pilot/t_mm

AE-705 Introduction to Flight Lecture 01 Capsule-01

Use the geometric altitude of the tables when referring to p,

density, and temp altitudes

Pressure altitude can be different from temp altitude and

density altitude and vice-versa

These altitude might differ from geometric altitude as well

Important points

AE-705 Introduction to Flight Lecture 01 Capsule-01

OTHER STANDARD ATMOSPHERES

USA, India, Arctic, Tropical, ….

AE-705 Introduction to Flight Lecture 01 Capsule-01

Other Standard Atmospheres

https://en.wikipedia.org/wiki/U.S._Standard_Atmosphere

1976 U.S. Standard Atmosphere

AE-705 Introduction to Flight Lecture 01 Capsule-01

https://www.google.com/search?q=united+states+standard+atmosphere+1976&source=lnms&tbm=isch&sa=X&sqi=2&ved=0ahUKEwjygv3XkJTUAhUMQo8KHeYeBl0Q_AUIBigB&biw=1570&bih=748#imgrc=hi4JaikQVNPzhM:&spf=1496027490886

1976 U.S. Standard Atmosphere cont..

AE-705 Introduction to Flight Lecture 01 Capsule-01

Indian Reference Atmosphere

Valid in Indian Equatorial Zone from Surface to 80 km Data recorded in 1985

Series of tables containing data related to • Temperature (K) • Pressure (millibars) • Density (kg m-3)

https://link.springer.com/article/10.1007%2Fs00382-016-3293-2

24

32

53

64

71

AE-705 Introduction to Flight Lecture 01 Capsule-01

https://link.springer.com/article/10.1007%2Fs00382-016-3293-2

Monthly temperature profiles from 14 years of observations (2002-15)

AE-705 Introduction to Flight Lecture 01 Capsule-01

Mumbai Weather Data (Nov 2016)

Actual Data

ISA

https://www.timeanddate.com/weather/india/mumbai/historic?month=11&year=2016

Hence, Mumbai atmosphere is

ISA +14

Elevation of

Mumbai is

14 m AMSL

AE-705 Introduction to Flight Lecture 01 Capsule-01

Minimum temperature (Antarctic) = -75 oC

Maximum temperature (Somalia, South Africa) = + 65 oC

Earth’s surface Temperature varies from -75 oC to + 65 oC

Temperature as Latitude

Arctic Minimum & Tropical Maximum

https://www.google.com/#q=arctic+minimum+atmosphere&spf=14968184947

50

AE-705 Introduction to Flight Lecture 01 Capsule-01

Q CODES FOR ALTITUDES

AE-705 Introduction to Flight Lecture 01 Capsule-01

QNH

1013.2

Flight level

1013.2

Height

elevation

QFE

MSL

QNH Altitude

• Pressure measured at ground reduced to MSL pressure

• Altitude displayed AMSL

station

AE-705 Introduction to Flight Lecture 01 Capsule-01

Runway (station)

29.92’’(1013.2 hpa ) Datum SL reference Datum (adjusted)

QFE

QNH

QNE

QFE & QNE

• SL pressure corrected for

temp for specific station

• height above the station

QFE

ISA mean atm pressure at SL

Referred as Standard

QNE

AE-705 Introduction to Flight Lecture 01 Capsule-01

Weather effects

AE-705 Introduction to Flight Lecture 01 Capsule-01

Weather Effects

Turbulence

Windshear

Clouds

Microburst

Rain & Hail