Preliminary Results of an Investigation by the Wing-Flow Method of the Longitudinal Stability Characteristics of a 1/50-Scale Semispan Model of the McDonnell XP-88 Airplane Metadata
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Title
- Main Title Preliminary Results of an Investigation by the Wing-Flow Method of the Longitudinal Stability Characteristics of a 1/50-Scale Semispan Model of the McDonnell XP-88 Airplane
- Series Title NACA Research Memorandums
Creator
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Author: Crane, Harold L.Creator Type: Personal
Contributor
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Originator: Langley Aeronautical LaboratoryContributor Type: OrganizationContributor Info: National Advisory Committee for Aeronautics. Langley Aeronautical Lab
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Originator: United States. Air Force. Air MateriƩl Command.Contributor Type: Organization
Date
- Creation: 1948-06-09
Language
- English
Description
- Content Description: "This paper presents the results of measurements of longitudinal stability of a 1/50-scale model of the XP-88 airplane by the wing-flow method. Lift, rolling-moment, hinge-moment, and pitching-moment characteristics as well as the downwash at the tail were measured over a Mach number range from approximately 0.5 to 1.05 at Reynolds numbers below 1,000,000. No measurements of drag were obtained" (p. 1).
- Physical Description: [27] p. : ill.
Subject
- Keyword: wing-flow method
- Keyword: aircraft stability
- Keyword: McDonnell XP-88
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/2060/20050028619
- Report No.: NACA-RM-SL8E28A
- Center for AeroSpace Information Number: 20050028619
- Archival Resource Key: ark:/67531/metadc64616