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goldenfox [79]
3 years ago
14

Choose a jet aircraft to use as your example for this activity. It should not be an exotic jet aircraft, as you will need to fin

d data online for the aircraft. If you choose a military aircraft, make sure you are not using classified data to support your work. Only use data that is available to all on the internet. You will then use the data you gathered for this particular aircraft to show examples of your performance problems and how you derived them.
To provide an outlook to some of the aspects of next module's unaccelerated performance, select a jet aircraft of your choice, choose three (3) of the following items of performance, and prepare an instructional presentation (utilizing a presentation tool of your choice - see resources in the Online Tools section) that explains in-depth how to find these different items of performance for a jet aircraft. This will be a standalone presentation and will not be attached to your comprehensive presentation project. Available choices:

maximum forward speed in level flight
absolute ceiling
best angle of climb airspeed
angle of climb
best rate of climb airspeed
rate of climb
maximum endurance airspeed
maximum range airspeed
influence of weight on performance
influence of altitude on performance
influence of configuration on performance
Engineering
1 answer:
matrenka [14]3 years ago
8 0

Answer:

burger piece waste that is waste waste waste waste please go back to your home

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Which of the following qualities of large man-made structures is unique to dams? They span water bodies They generate electricit
Anna11 [10]

They generate electricity.

8 0
3 years ago
Read 2 more answers
Consider a system whose temperature is 18°C. Express this temperature in R, K, and °F.
zvonat [6]

Answer:

In Rankine 524.07°R

In kelvin 291 K

In Fahrenheit 64.4°F  

Explanation:

We have given temperature 18°C

We have to convert this into Rankine R

From Celsius to Rankine we know that  T(R)=(T_{C}+273.15)\frac{9}{5}

We have to convert 18°C

So T(R)=(18+273.15)\frac{9}{5}=524.07^{\circ}R

Conversion from Celsius to kelvin

T(K)=(T_{C}+273)

We have to convert 18°C

T(K)=(18+273)=291K

Conversion of Celsius to Fahrenheit

T(F)=T_{C}\times \frac{9}{5}+32=64.4^{\circ}F

7 0
4 years ago
Explain the difference, on the basis of the test results, between the ultimate strength and the "true" stress at fracture.
gayaneshka [121]

Answer / Explanation:

On the basis of the test result, Ultimate strength which is mostly known as the ultimate tensile strength is the strength attached to the ability or capacity of a structural element or material used in the test to withstand elongation forces or pull force applied to it.  

WHILE,

True stress at fracture can be classified as stress or load associated to the point where yielding or fracture occurred divided by the cross-sectional area at the yield point.

5 0
3 years ago
Q.13 In order to produce maximum starting torque in a split-phase motor, how many degrees out of phase should the start- and run
Phantasy [73]

Answer:

D. 90 degrees.

Explanation:

Torque is a rotational force which moves an object in other direction. There should be 90 degrees out of phase to start, run winding currents with each other. Torque is produced by the rotational motion of an object. The angle of the object must be 90 degrees set in order to create torque.

3 0
3 years ago
A cylindrical specimen of cold-worked steel has a Brinell hardness of 250.(a) Estimate its ductility in percent elongation.(b) I
koban [17]

Answer:

A) Ductility = 11% EL

B) Radius after deformation = 4.27 mm

Explanation:

A) From equations in steel test,

Tensile Strength (Ts) = 3.45 x HB

Where HB is brinell hardness;

Thus, Ts = 3.45 x 250 = 862MPa

From image 1 attached below, for steel at Tensile strength of 862 MPa, %CW = 27%.

Also, from image 2,at CW of 27%,

Ductility is approximately, 11% EL

B) Now we know that formula for %CW is;

%CW = (Ao - Ad)/(Ao)

Where Ao is area with initial radius and Ad is area deformation.

Thus;

%CW = [[π(ro)² - π(rd)²] /π(ro)²] x 100

%CW = [1 - (rd)²/(ro)²]

1 - (%CW/100) = (rd)²/(ro)²

So;

(rd)²[1 - (%CW/100)] = (ro)²

So putting the values as gotten initially ;

(ro)² = 5²([1 - (27/100)]

(ro)² = 25 - 6.75

(ro) ² = 18.25

ro = √18.25

So ro = 4.27 mm

6 0
4 years ago
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