Experimental investigation at supersonic speeds of twin-scoop duct inlets of equal area 3: inlet enclosing 37.2 percent of the maximum circumference of the forebody Metadata
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Title
- Main Title Experimental investigation at supersonic speeds of twin-scoop duct inlets of equal area 3: inlet enclosing 37.2 percent of the maximum circumference of the forebody
- Series Title NACA Research Memorandums
Creator
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Author: Davis, Wallace F.Creator Type: Personal
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Author: Edwards, Sherman S.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: 1948-07-22
Language
- English
Description
- Content Description: Report presenting testing of a twin-scoop duct inlet that enclosed 37.2 percent of the forebody circumference at Mach numbers between 1.36 and 2.01. The approach to each scoop consisted of a ramp that deflected the flow to create an oblique shock wave in front of the duct entrance. Results regarding the inlet proportions, ramp angle, slots, and angle of incidence are provided.
- Physical Description: 25 p. : ill.
Subject
- Keyword: scoop duct inlets
- 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: 93R14746
- URL: http://hdl.handle.net/2060/19930085456
- Report No.: NACA-RM-A8E04
- Center for AeroSpace Information Number: 19930085456
- Archival Resource Key: ark:/67531/metadc57767
Note
- Display Note: "III."