Equasions Flashcards

1
Q

Track Error Angle =

A

(DOTX60)/D along trk

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2
Q

Max theoretical range=

A

1.23xsqrH1 + 1.23xsqrH2

H=feet
Range=NM

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3
Q

ILS GS exetremities?

A

Lower=0.45xG.P

Upper=1.75xG.P

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4
Q

Volts (V)=

A

IR

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5
Q

Power=

A

IV = Isq X R

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6
Q

Frequency (Hz)=

A

RPM X No pole pairs/ 60

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7
Q

Range (Land)=

Range (sea)=

A

2 X Sqr PWR (watts)

3 X sqr PWR (watts)

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8
Q

Power factor=

A

Kw (real/useful power)/Kva (total/apparent power)

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9
Q

PRF(pulse rep freq)=

A

1/PRP (pulse rep period)

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10
Q

Pulse radar max range (nm)=

A

C/2 x PRF

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11
Q

Minimum range of pulse radar (nm)=

A

C x pulse length/2

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12
Q

Thrust=

A

MV

Where V is the delta of air entering vs air exiting

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13
Q

Total thrust=

A

M(Vjet-Vflight)+A(pj-p0)

M = mass air flow
A = exhaust x section
V flight = TAS
VJet = exhaust velocity
Pj = exhaust static p
Po = Ambient static p
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14
Q

NAM=

A

NGM x TAS/GS

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15
Q

NGM (where TAS known)=

A

NAM x GS/TAS

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16
Q

NGM (TAS not known)=

A

NAM+/-(WCxtime)/60

Time in minutes

17
Q

Specific Air Range=

A

TAS/fuel flow

18
Q

Gross Fuel Flow=

A

Fuel flow/ground speed

19
Q

PSR=

A

E x H/
O + H

E = endurance in hours
O/H = ground speed
20
Q

PET=

A

D x H/
O + H

D = NM
O/H = ground speed
21
Q

RMS=

A

0.707 peak voltage

22
Q

QDM =

A

Hdg (M) + RB

23
Q

Rod for glide slope?

A

5 x GS x (gp/3)

24
Q

Change of RoD?

A

5 x change in gs

25
Q

Beam width =

A

70 x wavelength / dish diameter

26
Q

Displacement =

A

No cylinders x piston area x stroke (twice the throw)