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CRITICAL ANGLE ATTACK [3 records]

Record 1 2014-03-14

English

Subject field(s)
  • Aircraft Maneuvers
  • Aircraft Piloting and Navigation
DEF

A severe form of stall.

CONT

Stalls in airplane flight are often experienced as a sudden reduction in lift as the pilot brings the airplane to greater angle of attack and exceeds the critical(stall) angle of attack(which may be due to slowing down below stall speed). A stall of an airplane does not mean that its engines [have] stopped working, or that the airplane has stopped moving.

French

Domaine(s)
  • Manœuvres d'aéronefs
  • Pilotage et navigation aérienne
DEF

Cabrage d’un avion non provoqué par le pilote, qui peut se produire sous le seul effet de forces aérodynamiques et dans certaines plages de vitesse.

CONT

Autocabrage (pitch up) : C'est un phénomène d'instabilité longitudinale assez brutal, constaté sur les avions transsoniques à forte flèche, dans des circonstances réunissant Cz [coefficient de portance] et nombre de Mach assez élevé.

OBS

auto-cabrage : terme uniformisé par le Comité d'uniformisation de la terminologie aéronautique (CUTA) - Opérations aériennes.

OBS

cabrage non commandé : terme et définition publiés au Journal officiel de la République française le 21 décembre 2013.

Spanish

Save record 1

Record 2 2012-02-23

English

Subject field(s)
  • Aircraft Maneuvers
  • Aeroindustry
CONT

Separation occurs near the [leading] trailing edge when the stalling angle of attack is reached.

OBS

According to Jane's Aerospace Dictionary the term "critical angle" is incorrectly used to mean "stalling angle of attack".

French

Domaine(s)
  • Manœuvres d'aéronefs
  • Constructions aéronautiques
CONT

Le décollement se produit près du bord [d'attaque de fuite] lorsque l'angle de décrochage est atteint.

Spanish

Campo(s) temático(s)
  • Maniobras de las aeronaves
  • Industria aeronáutica
Save record 2

Record 3 2011-05-16

English

Subject field(s)
  • Helicopters (Military)
  • Aeronautical Engineering and Maintenance
CONT

The lower blade velocity of the retreating blade and the negative lift of the reverse flow region cause the outboard portion of the retreating blade to operate at higher and higher angles of attack as the aircraft forward flight speed is increased. At some airspeed, the retreating blade will surpass its critical stall angle of attack. This is referred to as retreating blade tip stall.

French

Domaine(s)
  • Hélicoptères (Militaire)
  • Aérotechnique et maintenance

Spanish

Save record 3

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