Longitudinal Stability Investigation of a Vertical-Take-Off-and-Landing Airplane Configuration With Simulated Jet Intake and Exhaust at Mach Numbers of 1.61 and 2.01 Metadata
Metadata describes a digital item, providing (if known) such information as creator, publisher, contents, size, relationship to other resources, and more. Metadata may also contain "preservation" components that help us to maintain the integrity of digital files over time.
- Main Title Longitudinal Stability Investigation of a Vertical-Take-Off-and-Landing Airplane Configuration With Simulated Jet Intake and Exhaust at Mach Numbers of 1.61 and 2.01
- Series Title NACA Research Memorandums
Author: Lord, Douglas R.Creator Type: Personal
Originator: Langley Aeronautical LaboratoryContributor Type: OrganizationContributor Info: National Advisory Committee for Aeronautics. Langley Aeronautical Lab
- Creation: 1958-01-30
- Content Description: Report presenting an investigation of a semispan model of a possible vertical-take-off-and-landing jet bomber configuration at a range of Mach numbers. The primary objective was to determine to the effects of jet interference, horizontal-tail location, and canard controls on the longitudinal stability characteristics of the model.
- Physical Description: 80 p. : ill.
- Keyword: VTOL aircraft
- Keyword: aircraft stability
- Keyword: aerodynamics
Name: National Advisory Committee for Aeronautics CollectionCode: NACA
Name: Technical Report Archive and Image LibraryCode: TRAIL
Name: UNT Libraries Government Documents DepartmentCode: UNTGD
- Rights Access: public
- Rights License: pd
- Rights Statement: No Copyright, Unclassified, Unlimited, Publicly available
- Accession or Local Control No: 93R19308
- URL: http://hdl.handle.net/2060/19930090018
- Report No.: NACA-RM-L57K05
- Center for AeroSpace Information Number: 19930090018
- Archival Resource Key: ark:/67531/metadc64021