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Test Q's
Choose one, please.
18. H540 CFI Which statement is true concerning the aerodynamic conditions which occur during a spin entry? A) After a full stall, both wings remain in a stalled condition throughout the rotation. B) After a partial stall, the wing that drops remains in a stalled condition while the rising wing regains and continues to produce lift, causing the rotation. C) After a full stall, the wing that drops continues in a stalled condition while the rising wing regains and continues to produce some lift, causing the rotation. |
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wrote in message ... Choose one, please. 18. H540 CFI Which statement is true concerning the aerodynamic conditions which occur during a spin entry? A) After a full stall, both wings remain in a stalled condition throughout the rotation. B) After a partial stall, the wing that drops remains in a stalled condition while the rising wing regains and continues to produce lift, causing the rotation. C) After a full stall, the wing that drops continues in a stalled condition while the rising wing regains and continues to produce some lift, causing the rotation. B |
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According to the Airplane Flying Handbook, FAA-H-8083-3, in its discussion
of spins, "the rising wing is less stalled than the descending wing..." which indicates to me that answer C is correct. "Less stalled than" means that some lift is being developed. This is not a black-and-white answer, though...it has been haggled over for decades. Bob Gardner wrote in message ... Choose one, please. 18. H540 CFI Which statement is true concerning the aerodynamic conditions which occur during a spin entry? A) After a full stall, both wings remain in a stalled condition throughout the rotation. B) After a partial stall, the wing that drops remains in a stalled condition while the rising wing regains and continues to produce lift, causing the rotation. C) After a full stall, the wing that drops continues in a stalled condition while the rising wing regains and continues to produce some lift, causing the rotation. |
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And I would read that as "both wings are stalled"... It's a very poorly
written question or very well written (depending on your point-of-view). I consider it poorly written because the answer is not clear in the training materials AND not clear on the exam. Chris Bob Gardner wrote: According to the Airplane Flying Handbook, FAA-H-8083-3, in its discussion of spins, "the rising wing is less stalled than the descending wing..." which indicates to me that answer C is correct. "Less stalled than" means that some lift is being developed. This is not a black-and-white answer, though...it has been haggled over for decades. Bob Gardner wrote in message ... Choose one, please. 18. H540 CFI Which statement is true concerning the aerodynamic conditions which occur during a spin entry? A) After a full stall, both wings remain in a stalled condition throughout the rotation. B) After a partial stall, the wing that drops remains in a stalled condition while the rising wing regains and continues to produce lift, causing the rotation. C) After a full stall, the wing that drops continues in a stalled condition while the rising wing regains and continues to produce some lift, causing the rotation. |
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This question has been on FAA knowledge exams since the 1960s, in one form
or another, and pilots have been trying to figure out what the FAA wants for at least that long. Bob Gardner "Chris G." nospam@noemail wrote in message eenews.net... And I would read that as "both wings are stalled"... It's a very poorly written question or very well written (depending on your point-of-view). I consider it poorly written because the answer is not clear in the training materials AND not clear on the exam. Chris Bob Gardner wrote: According to the Airplane Flying Handbook, FAA-H-8083-3, in its discussion of spins, "the rising wing is less stalled than the descending wing..." which indicates to me that answer C is correct. "Less stalled than" means that some lift is being developed. This is not a black-and-white answer, though...it has been haggled over for decades. Bob Gardner wrote in message ... Choose one, please. 18. H540 CFI Which statement is true concerning the aerodynamic conditions which occur during a spin entry? A) After a full stall, both wings remain in a stalled condition throughout the rotation. B) After a partial stall, the wing that drops remains in a stalled condition while the rising wing regains and continues to produce lift, causing the rotation. C) After a full stall, the wing that drops continues in a stalled condition while the rising wing regains and continues to produce some lift, causing the rotation. |
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ASA's Test Prep and "Stick and Rudder" say that Answer A is correct. Dunno
what Gleim says. Kershner says that both wings are stalled, but further on in the discussion he talks about "unequal lift." Hard to find an unequivocal answer. Bob Gardner wrote in message ... Choose one, please. 18. H540 CFI Which statement is true concerning the aerodynamic conditions which occur during a spin entry? A) After a full stall, both wings remain in a stalled condition throughout the rotation. B) After a partial stall, the wing that drops remains in a stalled condition while the rising wing regains and continues to produce lift, causing the rotation. C) After a full stall, the wing that drops continues in a stalled condition while the rising wing regains and continues to produce some lift, causing the rotation. |
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T o d d P a t t i s t wrote:
"Bob Gardner" wrote: ASA's Test Prep and "Stick and Rudder" say that Answer A is correct. Dunno what Gleim says. Kershner says that both wings are stalled, but further on in the discussion he talks about "unequal lift." Hard to find an unequivocal answer. I don't know the answer to this question, but I do know the following: 1) A stable spin mode can occur with both wings stalled, or only one. 2) Stalled wings always "produce lift." The deeper into the stall, the less lift they produce. If only slightly past the critical angle ("partially stalled"?) the wing produces nearly its max lift. If well past the critical angle ("full stall"?) it produces less, but it would "regain" lift if the angle decreased, even if it never actually unstalled. I'd probably call it drag rather than lift in a stall. :-) Having said that, I don't doubt for a minute that the wings will product unequal amounts of drag as the airplane descends in the spin. Matt |
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There is a movie documenting Richard Bach's late-70's barnstorming trip
around the country with a pair of Fleet biplanes (same name as the book, but I cannot remember what the title is). In one segment, he attaches flares to the wingtips and goes flying, ignites the flares and in the course of the flight, stalls and spins the aircraft. It is at this point the a picture makes clear what is happening with the wings. The smoke from the flare on the outside (flying) wing streams behind the wingtip, while the smoke from the flare on the inside (stalled) wing wafts slowly upward. This was filmed from the air from the accompanying aircraft. Chris G. wrote: And I would read that as "both wings are stalled"... It's a very poorly written question or very well written (depending on your point-of-view). I consider it poorly written because the answer is not clear in the training materials AND not clear on the exam. |
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