Study of Turning Performance of a Fighter-Type Airplane Particularly as Affected by Flaps and Increased Supercharging, Special Report Metadata
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Title
- Main Title Study of Turning Performance of a Fighter-Type Airplane Particularly as Affected by Flaps and Increased Supercharging, Special Report
- Series Title NACA Advanced Confidential Reports
- Series Title NACA Special Reports
Creator
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Author: Wetmore, J. W.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: 1942-06
Language
- English
Description
- Content Description: "Results of a study to determine the effects on turning performance due to various assumed modifications to a typical Naval fighter airplane are presented. The modifications considered included flaps of various types, both part and full space, increased supercharging, and increased wing loading. The calculations indicated that near the low-speed end of the speed range, the turning performance, as defined by steady level turns at a given speed, would be improved to some extent by any of the flaps considered at altitudes up to about 25,000 feet" (p. 1).
- Physical Description: [39] p. : ill.
Subject
- Keyword: aircraft stability
- Keyword: aircraft control
- Keyword: aircraft turning
Collection
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Name: National Advisory Committee for Aeronautics CollectionCode: NACA
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Name: Technical Report Archive and Image LibraryCode: TRAIL
Institution
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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
- URL: http://hdl.handle.net/2060/20090016589
- Report No.: NACA-ACR
- Report No.: NACA-SR-222
- Center for AeroSpace Information Number: 20090016589
- Archival Resource Key: ark:/67531/metadc65186