View source for Shock stalling

==English==

===Etymology===
From {{suffix|en|shock stall|ing|id2=gerund noun}}.

===Pronunciation===
* {{IPA|en|/ˈʃɒk ˌstɔːlɪŋ/|a=RP}}
* {{IPA|en|/ˈʃɑk ˌstɔlɪŋ/|a=GA}}
* {{hyphenation|en|shock stall|ing}}

===Noun===
{{en-noun}}

# {{lb|en|aviation}} {{gerund of|en|shock stall}}: the [[situation]] of [[undergo]]ing a [[shock stall]].
#* {{quote-journal|en|journal=The Journal of the Royal Aeronautical Society|location=London|publisher=w:Royal Aeronautical Society|year=1938|volume=42|page=226|issn=0368-3931|oclc=637686675|passage=That, of course, was perfectly true if one had the shock-stall over the complete aeroplane, but it seemed to him that the whole point of their study was to find out the causes of '''shock'''[-]'''stalling''' over small portions of the aeroplane, [...]}}
#* {{quote-book|en|author=staff of the RAE &#91;{{w|Royal Aircraft Establishment}}&#93; High Speed Wind Tunnel|title=High Speed Wind Tunnel Tests on Models of Two Jet-propelled Fighters (Meteor and Vampire)|series=[[w:Advisory Committee for Aeronautics|Aeronautical Research Council]] Reports and Memoranda|seriesvolume=no. 2504|location=London|publisher=[[w:Office of Public Sector Information|Her Majesty's Stationery Office]]|year=1951|page=35|oclc=30192878|passage=When the wing shock stalls, the lift gradient <math>a</math> falls and, if no '''shock stalling''' occurs on the tail plane, the term <math>\frac{a_1\bar{V}}{a}</math> increases, thus increasing the tail plane contribution to stability.}}
#* {{quote-book|en|author=[[w:Grigori Tokaty|G[rigori] A[leksandrovich] Tokaty]]|chapter=|title=A History and Philosophy of Fluid Mechanics|location=Henley-on-Thames, Oxfordshire|publisher=[[w:G. T. Foulis|G. T. Foulis & Co.]]|year=1971|page=220|oclc=873968059|newversion=reprinted|location2=New York, N.Y.|publisher2=w:Dover Publications|year2=1994|page2=220|pageurl2=https://books.google.com/books?id=ZmgJDgkDx8UC&pg=PA220|isbn2=978-0-486-68103-0|passage=Sometimes the pilot finds that his elevator or rudder is utterly ineffective. He moves the stick or the rudder pedals, but the aircraft fails to respond. This can be explained by the '''shock stalling''' of the fixed horizontal or vertical surfaces, in the presence of which the control surface moves in the wake and has no effect.}}

===Verb===
{{head|en|verb form}}

# {{infl of|en|shock stall||ing-form}}

{{cln|en|terms suffixed with -ing (participial)}}