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Darjan

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18 Questions

Votes Activity Newest Views

votes

answers

286

views

Why are lower VHF frequencies used for towers?

radio-communications frequency

Feb 20 at 13:28 Brian Drummond 1,298

votes

answers

187

views

Can Transition Altitude (TA) and Transition Level (TL) be equal?

air-traffic-control altitude

Nov 24 at 7:08 expeditedescent 33k

votes

answer

271

views

How are both squawk and altitude transmited when operating a Transponder in Mode C?

air-traffic-control radar transponder

Sep 20 at 19:21 DeltaLima 69.5k

vote

answers

121

views

Is it possible to have the laminar flow above $Re=10^7$?

aerodynamics fluid-mechanics fluid-dynamics flow

May 4 at 15:45 JZYL 10.3k

votes

answer

views

Why the gradient of $C_L$-$\alpha$ graph increases with the Mach number?

aerodynamics lift airfoil

Apr 18 at 19:01 JZYL 10.3k

votes

answers

views

How (and why) does engine thrust change with airspeed?

jet-engine aircraft-performance airspeed thrust

Mar 4 '20 at 21:42 Chuck MacLean 1

votes

answers

971

views

What is the difference between static and dynamic stall?

aerodynamics airfoil stall flight-dynamics fluid-dynamics

Mar 29 '19 at 21:38 Notts90 supports Monica 3,433

vote

answers

views

What is subcritical and supercritical boundary layer?

aerodynamics airfoil flow

Feb 10 '19 at 19:12 Darjan 958

vote

answers

904

views

Why does an aircraft's nose tend to pitch downward at higher bank angles?

aerodynamics weight-and-balance pitch roll flight-mechanics

Jan 31 '19 at 23:12 Andrius 3,641

-1

votes

answer

views

Hydromechanical/Electronic fuel control system [closed]

aircraft-systems engine fuel-systems propulsion airframe-and-powerplant

Jan 27 '19 at 17:36 John K 81.9k

votes

answers

views

What is a rudder or fin stall?

aerodynamics airfoil stall vertical-stabilizer flight-mechanics

Jan 25 '19 at 1:53 Robert DiGiovanni 9,498

votes

answers

views

Why is Reverse thrust more effective at higher airspeeds?

landing aircraft-physics thrust-reverser

Jan 9 '19 at 12:37 Mike Sowsun 28.5k

votes

answer

275

views

Why does strong shock wave-boundary-layer interaction produce a bubble reattachment?

aerodynamics airfoil supersonic fluid-mechanics shock-waves

Dec 29 '18 at 5:04 Pondlife 63.9k

vote

answer

134

views

Is high speed buffet possible at supersonic speed?

airfoil supersonic fluid-mechanics shock-waves

Nov 20 '18 at 3:25 Peter Kämpf 200k

vote

answer

views

What is primary cause of shock induced separation (shock stall)?

aerodynamics supersonic stall shock-waves

Oct 18 '18 at 16:34 ares 604

votes

answers

608

views

Transonic buffet - reason for a rapid movements of the shockwave along the wing chord line?

aerodynamics airfoil shock-waves transonic fluid-dynamics

Oct 5 '18 at 19:20 Robert DiGiovanni 9,498

votes

answer

590

views

Why is the delta wing naturally stable in pitch?

aerodynamics stability fluid-mechanics delta-wing fluid-dynamics

Sep 28 '18 at 22:11 Darjan 958

votes

answer

398

views

What is the fuel mass flow rate at stationary full power for the CFM56 5C2/3C1 engines?

engine fuel turbofan fuel-consumption flow

Apr 4 '18 at 2:02 ymb1 99.5k

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18 Questions

Why are lower VHF frequencies used for towers?

Can Transition Altitude (TA) and Transition Level (TL) be equal?

How are both squawk and altitude transmited when operating a Transponder in Mode C?

Is it possible to have the laminar flow above $Re=10^7$?

Why the gradient of $C_L$-$\alpha$ graph increases with the Mach number?

How (and why) does engine thrust change with airspeed?

What is the difference between static and dynamic stall?

What is subcritical and supercritical boundary layer?

Why does an aircraft's nose tend to pitch downward at higher bank angles?

Hydromechanical/Electronic fuel control system [closed]

What is a rudder or fin stall?

Why is Reverse thrust more effective at higher airspeeds?

Why does strong shock wave-boundary-layer interaction produce a bubble reattachment?

Is high speed buffet possible at supersonic speed?

What is primary cause of shock induced separation (shock stall)?

Transonic buffet - reason for a rapid movements of the shockwave along the wing chord line?

Why is the delta wing naturally stable in pitch?

What is the fuel mass flow rate at stationary full power for the CFM56 5C2/3C1 engines?