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Random Deviations from Cruise Altitudes of a Turbojet Transport at Altitudes of a Turbojet Transport at Altitudes between 20,000 and 41,000 FeetAn evaluation has been made of the random deviations from the cruise altitudes (called flight technical error) of a large turbojet transport on scheduled, passenger-carrying operations over the Eastern United States, the Atlantic Ocean, and Western Europe. Data were collected from l9O flights through an altitude range of 20,000 to 41,000 feet and for a time period from January to August 1959. The results of the investigation, based on an evaluation of the altitude recordings of an NASA VGH recorder, showed that for a high percentage of the total cruise time (99.0 percent) the airplane operated within 100 feet of its stabilized cruise altitude. On occasion, however, the excursions of the airplane from the cruise altitude reached large values (in excess of 1,000 feet in the worst case).
Document ID
20040047100
Acquisition Source
Headquarters
Document Type
Other - NASA Technical Note (TN)
Authors
Gracey, William
(NASA Langley Research Center Hampton, VA, United States)
Shipp, Jo Ann
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 21, 2013
Publication Date
April 1, 1961
Subject Category
Aircraft Stability And Control
Report/Patent Number
L-1465
NASA-TN-D-820
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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