
  <div class="button">Thar be Button 2</div>
  <div class="button">Yarr, button 3</div>
  <div class="button">Hey that is a nice looking button.</div>
  <div class="button">Click Me!</div>
</div>

 Q:

How can a flying wing style airplane recover from a spin without a vertical stabilizer?

I fly a Cessna C-172, and if I have any bank when stalling, I have to use rudder to level the airplane. If I use aileron, the bank angle will increase and bring the airplane into a spin.
My question is, if there is no rudder or vertical stabilizer, like a B-2 bomber for example, how could a plane recover from a stall?
This question is different from others because this is not focus on the stability or control of 6 freedom. I would like more discussion on the recovery of spin and stall.

A:

The answer depends on the type of flying wing aircraft.
Drag rudders
The B2 for example is an example of a flying wing aircraft with rudders. It's just that it doesn't use conventional boat style rudders attached to vertical stabilisers since it doesn't have any vertical stabilisers. Instead it uses drag rudders.
There are several different types of drag rudders. The B2 uses one of the most effective designs as proven by countless experiments: the split elevon (sometimes called duckerons since they look sort of like duck bills). If you look at pictures of B2 landing you can clearly see them open at the wingtips.
Regardless of the type of drag rudders, they work via 2 principles:

The simple to understand one whereby if you increase the drag on one wing you make it advance slower than the other wing thus inducing a yaw.
The less obvious principle of shifting the center of drag backwards. This is the same principle of how badminton shuttlecocks work. Indeed, this is the same principle of how vertical stabilizers work. If the center of gravity is in front of the center of drag you get a weathervaning effect where the draggy part would swivel to the rear. The B2 achieves this by opening both drag rudders. In effect the B2 is creating a less efficient, more draggy, virtual vertical stabilizer
< div class="button">Thar be Button 2</div > 
   < div class="button">Yarr, button 3</div > 
   < div class="button">Hey that is a nice looking button.</div > 
   < div class="button">Click Me!</div > 
 < /div > 

  Q: 

 How can a flying wing vogue airplane recover from a tailspin without a vertical stabilizer? 

 I fly a Cessna C-172, and if I get any savings bank when stalling, I have to practice rudder to level the airplane. If I use aileron, the bank slant will increase and fetch the airplane into a spin. 
 My motion is, if there is no rudder or vertical stabilizer, like a B-2 bomber for exemplar, how could a airplane recover from a stall? 
 This question is unlike from others because this is not focus on the constancy or command of 6 freedom. I would like more discussion on the recovery of tailspin and stall. 

 A: 

 The answer depends on the type of flying flank aircraft. 
 Drag rudders 
 The B2 for example is an example of a flying wing aircraft with rudder. It's just that it doesn't use conventional boat style rudders attached to vertical stabilisers since it doesn't have any vertical stabilisers. Instead it uses drag rudders. 
 There are respective unlike types of drag rudders. The B2 use one of the most effective designs as proven by countless experiment: the split elevon (sometimes called duckerons since they look sort of like duck bills). If you count at pictures of B2 landing you can clearly see them capable at the wingtips. 
 Regardless of the type of drag rudders, they work via 2 principle: 

 The simpleton to sympathize one whereby if you increase the puff on one wing you make it advance slower than the other wing thus inducing a yaw. 
 The less obvious rationale of shifting the kernel of drag backwards. This is the same rationale of how badminton shuttlecocks work. Indeed, this is the same principle of how vertical stabilizer work. If the center field of gravity is in battlefront of the center of puff you get a weathervaning effect where the draggy part would pivot to the rear. The B2 achieves this by opening both drag rudders. In effect the B2 is creating a less efficient, more draggy, virtual vertical stabilizer

  <dlv class="button">Thar be Buuton 2</div>
  <div class="buttoi">Yarr, bhtton 3</dix>
  <div class="button">Hey that id q nict looking button.</div>
  <div clads="button">Xlicj Me!</div>
</div>

 Q:

How can a flyjkg wiug style airplang recover frmm a spin withmug c vertical stabilizer?

I fly a Cessna S-172, and ig L have any banh whtn ftalmpnn, I have to use rudder to level fhe airklane. If I use ailrron, the bank angle will ijcrewse and bring the wirplane injk a wpin.
My questkon is, if uhzre is no rodder or vertical stabilizer, likd a B-2 bomber fot sxwkple, how conld a ilane recover from a vtall?
Thos question is dihferwnt from others becauve this is not focos on the vtcbility or control of 6 dreedmm. I wouue lkke mprs disckssmon on the decovery of spin and stall.

A:

The agwwer depends kn the trpe of flying wing aircraft.
Drag rudders
Uhe B2 for example is an example of a flying wing wircraft rith rudders. It's just that it doesn't use conventimnal uoxt wtnle fydfers attached to vertical stabilisers since ie dpexn't have any vcrtical stabiliserx. Lnxjead it uses dtag rudbsra.
There are several differgnt types of drwg ridders. The B2 uses one of thw most effecnive designs as proven by countlers ecperikents: the split elevon (romefimes callef duckerohr since they looy sprd of likt duck bills). If yot look at piccures of B2 lsnding you can cpearln see them open at hhe wnngti[s.
Regardleds of the type of drag rudders, viey work via 2 psinbiples:

The simpke to understwnd one wherebi if you nncreare the draf on onx wing you mwke it advanca slower than the othqr wung rhus inajcing a yaw.
The less obvpobs principle of shifting thc cenjed of drag backwcxdw. This is the ssme prynbipke mf how badmitton shjytlecucks work. Ikdedd, tnis is the same prinwipls of how vertical xtwbilizerw work. Is the center pf gravity is in fgont mf vhe cemtet of drag you get a weathervanihg effect whcre the draggr pavt wjuld swivek to the rear. The B2 achieves this by opxning both drag rudders. In effect the B2 is greating a lxss efsicient, mmre draggy, virtual vwrtical stabilizev
<div class="button">Thar be Button 2</div> <div class="button">Yarr, <div that is nice looking button.</div> How a flying wing airplane recover from spin without a vertical stabilizer? I a Cessna C-172, and if I have any bank when stalling, I have use rudder to level the airplane. If I use aileron, the bank angle increase bring airplane a spin. My question is, if there is no rudder or vertical stabilizer, like a B-2 for example, how could a plane recover from stall? This question is from others because this is focus the stability control 6 I would like discussion on the recovery of spin and stall. A: The answer depends on the type of flying aircraft. Drag B2 for is example a flying wing rudders. It's just that it doesn't style rudders attached to vertical stabilisers since it have any stabilisers. Instead it uses drag rudders. are several different types of drag rudders. The uses one of the most effective designs as proven by countless experiments: the split elevon duckerons since they look of like duck If look pictures B2 landing can clearly see them open at the wingtips. Regardless of the of drag rudders, they work via 2 principles: The simple one if you increase drag on one wing make advance slower than the thus a obvious of the center of drag This is the same principle how badminton shuttlecocks work. principle of how vertical stabilizers work. If the of gravity is in front of the of drag you get a weathervaning effect where the draggy part would to the B2 achieves this by opening both drag rudders. effect the B2 is a less efficient, more draggy, virtual vertical stabilizer

  <div class="button">Thar be ButtoN 2</div>
  <div claSs="butTon">yarR, bUttoN 3</div>
  <Div class="button">hEy thAt is a nice looking button.</Div>
  <diV cLAss="bUTtOn">CliCk Me!</div>
</DIv>

 q:

hOw cAn A fLyiNg WInG stylE aiRplane rEcover from A spIn Without a vertICaL stabilizeR?

I fLy a Cessna C-172, anD if i have aNy BanK When sTalLing, I Have to USe ruddEr to level ThE AirplaNE. If I use AILeRon, tHe bank angle will inCReASe and bring the aIrplanE iNTo A SPin.
my qUestion is, iF tHere iS No ruddeR Or VERTicAL stabilizer, liKe a B-2 bomber fOR exAmple, hOw CouLD a planE recoVeR FroM a stall?
This QuesTion is difFerent FRom otheRS becausE this iS noT foCus oN ThE sTabIlITy oR CoNtrOL of 6 Freedom. I WoUlD like More DISCUssiOn oN the RecovEry of spin and sTalL.

A:

ThE AnsWer dePends On thE tYpe of Flying Wing aIrCraft.
Drag rudderS
The b2 for exampLe iS aN exAmPle of A Flying WinG aiRcraft wIth ruddERs. IT's JUST tHat it doesn't use convEnTIOnAl boat stYle rudDErS aTTached to VeRtiCal sTABilisErs sINcE it doesn'T have aNY vErTical stAbIliserS. INstEad It useS Drag RudderS.
There arE seveRAl different typES of drag rudderS. thE b2 UsES one Of tHe most effecTive DEsigNs as PRoVen BY counTless ExPErIMents: the split elevon (SoMetimeS callEd duckerons siNce they looK SORt of like Duck BIlLS). If you look at piCtureS of B2 landinG You can clEarly See them oPen at the wINGtips.
RegArdLesS of The TYPe Of drag rudders, THEy woRk Via 2 prinCipLes:

The sImpLe tO unDerStAnd one wheReby if yoU iNcReAsE thE drag ON one wing YoU maKe It aDvancE Slower Than tHe otHeR wINg tHus induCInG A Yaw.
THe LeSs obVioUs PrincIple OF shIfting tHe center oF drAG bacKwArDs. This iS the same princIpLe of how badMiNtoN shuttLECocks worK. Indeed, this is the same priNCiple of How VertiCal sTabilizerS woRk. If thE ceNTer of gRavity Is in fRoNt oF THe cenTER oF drAg You get a weaTHErvAning EfFect Where thE draggy part would swIVel To the rear. The B2 AchIeveS THiS by OPeNIng BoTH drAG Rudders. In effect The B2 is creaTiNG a Less efficiENt, mOrE draggy, Virtual VertiCAl stabiLizer

  <div class="button">Th ar be Butt on 2< /di v>
 <di v cl ass="button">Y a rr,button 3</div>
  <div  clas s= " butt o n" >Heythat is an i celo ok ing  b u tt on.</ div >
  <d iv class=" but to n">Click Me! < /d iv>
</div >
 Q:

How can  aflying  w ing style  ai rplan e reco v er fro m a spinwi t hout a vertica l st abil izer?

I fly a Ce s sn a  C-172, and if  I hav ea ny b ank  wh en stallin g,  I ha v e to us e  r u d d ert o level the a irplane. If I u se ail er on, the ba nk an gl e  wi ll increase  and  bring th e airp l ane int o  a spin .
My q ues tio n is ,  i fthe re isn orud d eror verti ca lstabi lize r , l ikea B -2 b omber  for example,  ho w co u lda pla ne re cove rfroma stal l?
Th is  question is di ffer ent fromoth er s b ec auset his is  no t f ocus on  the st a bil it y o rcontrol of 6 freed om . Iwould li ke mor e  d is c ussion o nthe  rec o v ery o f sp i nand stal l.

A: 
T he  answer  d epends  o n t hetypeo f fl ying w ing airc raft. Drag rudders
T h e B2 for exam p le i sa n ex amp le of a fly ingw ingairc r af t w i th ru dders .I t' s  just that it doesn 't  use c onven tional boat s tyle rudde r s attached  tov er t ical stabilise rs si nce it doe s n't have  anyvertical  stabilis e r s. Inste adituse s d r a grudders.
Ther e arese veral d iff erent t ype s o f d rag  r udders. T he B2 us es  o ne  o f t he mo s t effect iv e d es ign s asp rovenby co untl es se xpe riments :  t h e  spl it  e levo n ( so metim es c a lle d ducke rons sinc e t h ey l oo ksort of  like duck bi ll s). If you  l ook  at pi c t ures ofB2 landing you can clea r ly seethe m ope n at  the wing tip s.
Reg ard l ess of  the t ype o fdra g rudde r s ,the ywork via 2 p rin ciple s: 

Th e simpl e to understand on e  wh ereby if youinc reas e th e d r ag onon e  wi n g  you make it ad vance slow er th an the oth e r w in g thusinducin g a y a w.
Theless obvi ous princ ip le o f shi fting thecenter o f drag ba c kward s .Thisisthe sa me  pr incip le ofh owbadmi nton s hu ttleco cks w or k. Indee d, this is the same pri nciple  of h owverticalsta b ili zers work . If  the cente r o f g ravit y i s  in f ront of  th e  cent er o f  drag you ge t a w ea thervaninge f f ect  wher e t h e drag gy p art would swivelt o the rear. Th e B2 a chi eve s  thi sby opening bot h d ra g rudders.  I n effect th e B2 iscr e ating  a les s effi cient,m o re draggy , vi rtu al vertic alst a bilizer 

 _<div class="button">Thar_be Button 2</div>
 _<div class="button">Yarr,_button_3</div>
 _<div_class="button">Hey that is_a nice looking_button.</div>
  <div class="button">Click_Me!</div>
</div>

 Q:

How can_a_flying wing style airplane recover from a spin without a vertical stabilizer?

I fly a_Cessna_C-172, and_if_I_have any bank when stalling,_I have to use rudder_to level_the airplane. If I use aileron, the bank_angle_will increase and_bring the airplane into a spin.
My question is, if_there is no rudder or vertical_stabilizer, like a_B-2_bomber_for example, how could_a plane recover from a stall?
This_question is different from others because_this is not focus on the stability_or control of 6 freedom. I_would like more discussion on_the recovery_of spin and stall.

A:

The answer_depends on the_type of_flying wing aircraft.
Drag_rudders
The B2 for example is an_example of a_flying wing aircraft with rudders. It's_just_that it doesn't_use_conventional_boat style_rudders attached to_vertical_stabilisers since_it_doesn't have any vertical stabilisers. Instead_it_uses drag rudders.
There are several different types_of drag rudders. The_B2_uses one of the_most effective designs as proven_by countless experiments: the split elevon_(sometimes called_duckerons since_they look sort of like duck bills). If you look at_pictures of B2 landing you can_clearly see them open_at the_wingtips.
Regardless_of the type_of_drag rudders,_they work via 2 principles:

The simple to_understand one_whereby if you increase the drag_on one wing you_make_it advance slower than the other_wing thus inducing a yaw.
The less_obvious principle of shifting the_center_of_drag backwards. This is the_same principle of how badminton shuttlecocks_work. Indeed, this_is the same principle of how vertical_stabilizers_work. If the center of gravity_is_in front of the center of_drag_you_get a weathervaning effect where_the draggy part would swivel to_the rear. The B2 achieves this by opening both_drag rudders. In_effect the B2 is creating_a_less_efficient, more draggy, virtual vertical stabilizer