A flight investigation at transonic speeds of a model having a triangular wing of aspect ratio 3 Metadata
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Title
- Main Title A flight investigation at transonic speeds of a model having a triangular wing of aspect ratio 3
- Series Title NACA Research Memorandums
Creator
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Author: White, Maurice D.Creator Type: Personal
Contributor
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Originator: Ames Aeronautical Laboratory (U.S.)Contributor Type: OrganizationContributor Info: National Advisory Committee for Aeronautics. Ames Aeronautical Lab
Date
- Creation: 1955-06-24
Language
- English
Description
- Content Description: Report presenting free-falling recoverable-model tests at transonic speeds on a model with a triangular wing of aspect ratio 3 and a 45 degree swept tail located in the chord plane of the wing. Static and dynamic longitudinal-stability data for the complete model, force and moment data for the major components of the model, and load distributions over the fuselage of the model were evaluated at a range of angles of attack. results regarding lift, drag, static longitudinal stability, dynamic longitudinal stability, horizontal-tail effectiveness, loading distributions over fuselage, and buffet boundary are provided.
- Physical Description: 39 p. : ill.
Subject
- Keyword: triangular wings
- Keyword: aircraft stability
- Keyword: aerodynamics
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
- Accession or Local Control No: 93R17956
- URL: http://hdl.handle.net/2060/19930088666
- Report No.: NACA-RM-A55D18
- Center for AeroSpace Information Number: 19930088666
- Archival Resource Key: ark:/67531/metadc61266