Boeing 707 Barrell Roll
#1 Posted 07 February 2013 - 02:55 AM
#2 Posted 07 February 2013 - 03:34 AM


Alexxander "Tigerwolf" Vandross
118th Fighter Wing Razor Squadron CO/Phantom 4
1/10/50/200/500/2000/10000 Yes, there are over 11,050 beta keys left at mmorpg . com
Vice President & Co-Founder of FRAG: We haz BETA GALs
#4 Posted 07 February 2013 - 06:31 AM


Per Ardua ad Astra
"Through Adversity to the Stars"
Royal Australian Air Force
#6 Posted 07 February 2013 - 01:39 PM
I'd love it.
#7 Posted 07 February 2013 - 04:13 PM
They landed OK, but the elevators were shot.
#8 Posted 07 February 2013 - 04:18 PM


We the willing, led by the unknowing, continue to do the impossible for the ungrateful
#9 Posted 07 February 2013 - 08:34 PM
planogram, on 07 February 2013 - 11:42 AM, said:
Well i have enough fuel in the engine fuel reservoir for the maneuver, and its fuel injected not a carbie, i can use the aux fuel pump if i have to.


Per Ardua ad Astra
"Through Adversity to the Stars"
Royal Australian Air Force
#10 Posted 07 February 2013 - 10:54 PM


******************************************* Fail to Suck ****************************************
#11 Posted 08 February 2013 - 01:58 AM
MacMyers, on 07 February 2013 - 10:54 PM, said:
Why would you say that? In fact the wings would not fall off, planes are built a little tougher than that

#12 Posted 08 February 2013 - 03:03 AM
AlexVandross, on 07 February 2013 - 03:34 AM, said:
To my knowledge, a 747 has never been barrel rolled at an airshow. There was a crazy B-52 pilot at Fairchild AFB a while back who thought his B-52 was an F-16. He thought this so much so that he decided to prove it.....until he augered into the ground from an unrecoverable high-bank turn.
Crag_r, on 07 February 2013 - 06:31 AM, said:
This is true. A properly executed barrel roll is a continuous 1-G maneuver, since you're continuously applying back pressure throughout the maneuver.
planogram, on 07 February 2013 - 11:42 AM, said:
Regardless if it had a gravity fed system or required a fuel pump, so long as positive Gs were applied to the aircraft, fuel will still feed to the engine. The issue comes when you start applying negative Gs to an aircraft that is not fuel-injected.
A perfect example of this is early-Mk. Spitfires vs. Messerschmitt Bf.109s during the Battle of Britain. Bf.109s were fuel-injected, while Spitfires were not. When being pursued by a Spitfire, a 109 pilot would simply push the stick forward and enter a steep dive. If the Spit pilot did this, they would un-port the fuel and potentially cause their engine to seize. To alleviate this, the Spit pilot could roll inverted and pull on the stick, causing positive Gs and allowing them to continue the pursuit.
MacMyers, on 07 February 2013 - 10:54 PM, said:
A 1-G maneuver causes no significant additional stress to the aircraft. What you're thinking of is a term called Load Factor. Load factor is the total amount of lift the aircraft is producing divided by the aircraft's weight, which is expressed in the term "Gs".
In level flight, an aircraft's total lift equals its weight. However, when an aircraft enters a level turn, its vertical component of lift now equals its weight. In order to create enough vertical lift to equal its weight, the aircraft has to create more total lift. This total lift (and equal but opposite "resultant force") now gets divided by the aircraft's weight, which results in the aircraft's Load Factor.
Any time an aircraft produces more total lift than the aircraft's weight, it experiences a Load Factor of more than 1. For example, a level 60 degree bank turn equals 2Gs. A 70 degree bank turn is 3Gs. Keep in mind, however, that lift is always relative to the aircraft's flight path, and not necessarily in which direction the nose is pointed. But I digress...
Suffice to say that a discussion on Load Factor is best done in a classroom (with a lot of markerboards and multiple colored markers). A forum? Not the greatest locale.

FAA Airline Transport Pilot, Dash 8 Type Rating
Certified Flight Instructor -- Airplane - Single-Engine, Airplane - Multi-Engine, Instrument - Airplane
7,000+ flight hours -- Low-Vis, CAT III, Mountainous Terrain, High Traffic, International
#13 Posted 08 February 2013 - 06:08 AM
gaidalcain85, on 08 February 2013 - 01:58 AM, said:
Heh... OK trying flying one upside down for awhile. I'm not talking about a G controlled roll.


******************************************* Fail to Suck ****************************************
#15 Posted 18 February 2013 - 08:18 PM
CrashTailspin, on 08 February 2013 - 03:03 AM, said:
To my knowledge, a 747 has never been barrel rolled at an airshow. There was a crazy B-52 pilot at Fairchild AFB a while back who thought his B-52 was an F-16. He thought this so much so that he decided to prove it.....until he augered into the ground from an unrecoverable high-bank turn.
This is true. A properly executed barrel roll is a continuous 1-G maneuver, since you're continuously applying back pressure throughout the maneuver.
Regardless if it had a gravity fed system or required a fuel pump, so long as positive Gs were applied to the aircraft, fuel will still feed to the engine. The issue comes when you start applying negative Gs to an aircraft that is not fuel-injected.
A perfect example of this is early-Mk. Spitfires vs. Messerschmitt Bf.109s during the Battle of Britain. Bf.109s were fuel-injected, while Spitfires were not. When being pursued by a Spitfire, a 109 pilot would simply push the stick forward and enter a steep dive. If the Spit pilot did this, they would un-port the fuel and potentially cause their engine to seize. To alleviate this, the Spit pilot could roll inverted and pull on the stick, causing positive Gs and allowing them to continue the pursuit.
A 1-G maneuver causes no significant additional stress to the aircraft. What you're thinking of is a term called Load Factor. Load factor is the total amount of lift the aircraft is producing divided by the aircraft's weight, which is expressed in the term "Gs".
In level flight, an aircraft's total lift equals its weight. However, when an aircraft enters a level turn, its vertical component of lift now equals its weight. In order to create enough vertical lift to equal its weight, the aircraft has to create more total lift. This total lift (and equal but opposite "resultant force") now gets divided by the aircraft's weight, which results in the aircraft's Load Factor.
Any time an aircraft produces more total lift than the aircraft's weight, it experiences a Load Factor of more than 1. For example, a level 60 degree bank turn equals 2Gs. A 70 degree bank turn is 3Gs. Keep in mind, however, that lift is always relative to the aircraft's flight path, and not necessarily in which direction the nose is pointed. But I digress...
Suffice to say that a discussion on Load Factor is best done in a classroom (with a lot of markerboards and multiple colored markers). A forum? Not the greatest locale.


President and Founder of FRAG
#16 Posted 18 February 2013 - 08:25 PM
Sgt_Goldham, on 18 February 2013 - 07:50 PM, said:
Heheh... yeah... but the aircraft is not designed to take said G's on the top of the control surfaces. If you try to fly most aircraft inverted the wings will come off. Quite rapidly in fact.
Try it it if you don't believe me.


******************************************* Fail to Suck ****************************************
#17 Posted 18 February 2013 - 08:42 PM
MacMyers, on 18 February 2013 - 08:25 PM, said:
Try it it if you don't believe me.


President and Founder of FRAG
#18 Posted 18 February 2013 - 11:32 PM
MacMyers, on 18 February 2013 - 08:25 PM, said:
Try it it if you don't believe me.
My god!
You put the same load on the wings flying inverted as you do flying level, the only difference is because the airfoil is upside down the aircraft is going to want to pull down as opposed to up (most aircraft). The Extra 300's wings are designed with zero incidence, so it will fly equally as good upside down as it would right side up.
Basically what Crash said is completely correct, as he is a pilot, and I as well am a pilot. We have to learn this stuff from day one.

Proof of Ace: A6M2 A6M5 F4F F2G P-51A
#19 Posted 19 February 2013 - 02:59 AM
MacMyers, on 18 February 2013 - 08:25 PM, said:
Try it it if you don't believe me.
You only have -1G while flying inverted in Level flight, legally in order for an Aircraft to be Airworthy (for the most part) it has to be able to easily cope with that.
So no the wings will not fall off, remember wings are VERY strong things they take the entire weight of the Aircraft in the Air.


Per Ardua ad Astra
"Through Adversity to the Stars"
Royal Australian Air Force
#20 Posted 19 February 2013 - 04:42 AM
I guess it depends on your definition of "flying inverted"


******************************************* Fail to Suck ****************************************








