A method of calibrating airspeed installations on airplanes at transonic and supersonic speeds by the use of accelerometer and attitude-angle measurements Metadata
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- Main Title A method of calibrating airspeed installations on airplanes at transonic and supersonic speeds by the use of accelerometer and attitude-angle measurements
- Series Title NACA Technical Reports
Author: Zalovick, John A.Creator Type: Personal
Author: Lina, Lindsay J.Creator Type: Personal
Author: Trant, James P., Jr.Creator Type: Personal
Originator: Langley Aeronautical LaboratoryContributor Type: OrganizationContributor Info: National Advisory Committee for Aeronautics. Langley Aeronautical Lab
- Creation: 1952-12-05
- Content Description: A method is described for calibrating airspeed installation on airplanes at transonic and supersonic speeds in vertical-plane maneuvers in which use is made of measurements of normal and longitudinal accelerations and attitude angle. In this method all the required instrumentation is carried within the airplane. An analytical study of the effects of various sources of error on the accuracy of an airspeed calibration by the accelerometer method indicated that the required measurements can be made accurately enough to insure a satisfactory calibration.
- Physical Description: 13 p. : ill.
- Keyword: airspeed installation
- Keyword: pitot-static installation
Name: National Advisory Committee for Aeronautics CollectionCode: NACA
Name: Technical Report Archive and Image LibraryCode: TRAIL
Name: UNT Libraries Government Documents DepartmentCode: UNTGD
- Rights Access: public
- Rights License: pd
- Rights Statement: No Copyright, Unclassified, Unlimited, Publicly available
- Accession or Local Control No: 93R21464
- URL: http://hdl.handle.net/2060/19930092174
- Report No.: NACA-TR-1145
- Center for AeroSpace Information Number: 19930092174
- Archival Resource Key: ark:/67531/metadc60513