Langley Free-Flight-Tunnel Investigation of the Automatic Lateral Stability Characteristics of a Model Equipped with a Gyro Stabilizing Unit that Provided either Flicker-Type or Hunting Control Metadata
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Title
- Main Title Langley Free-Flight-Tunnel Investigation of the Automatic Lateral Stability Characteristics of a Model Equipped with a Gyro Stabilizing Unit that Provided either Flicker-Type or Hunting Control
- Series Title NACA Research Memorandums
Creator
-
Author: Schade, Robert O.Creator Type: Personal
Contributor
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Originator: Langley Aeronautical LaboratoryContributor Type: OrganizationContributor Info: National Advisory Committee for Aeronautics. Langley Aeronautical Lab
Date
- Creation: 1949-01-11
Language
- English
Description
- Content Description: Memorandum presenting an investigation to determine the automatic lateral stability characteristics of a model equipped with a gyro stabilizing unit that gave response to bank and yaw. Stable flights were obtained with the flicker-type automatic control, and the amplitude of the oscillations was decreased by adding the attachment which provided hunting control.
- Physical Description: 39 p. : ill.
Subject
- Keyword: aircraft stability
- Keyword: gyro stabilizing units
Collection
-
Name: National Advisory Committee for Aeronautics CollectionCode: NACA
-
Name: Technical Report Archive and Image LibraryCode: TRAIL
Institution
-
Name: UNT Libraries Government Documents DepartmentCode: UNTGD
Rights
- Rights Access: public
- Rights License: pd
- Rights Statement: No Copyright, Unclassified, Unlimited, Publicly available
Resource Type
- Report
Format
- Text
Identifier
- Accession or Local Control No: 93R14779
- URL: http://hdl.handle.net/2060/19930085489
- Report No.: NACA-RM-L8K04
- Center for AeroSpace Information Number: 19930085489
- Archival Resource Key: ark:/67531/metadc57826