Research Catalog

Investigation of two bifurcated-duct inlet systems from Mach 0 to 2.0 over a wide range of angles of attack

Title
Investigation of two bifurcated-duct inlet systems from Mach 0 to 2.0 over a wide range of angles of attack / Eldon A. Latham.
Author
Latham, Eldon A.
Publication
Moffett Field, California : Ames Research Center, May 1976.

Available Online

https://purl.fdlp.gov/GPO/gpo171204

Details

Additional Authors
  • Ames Research Center, issuing body.
  • United States. National Aeronautics and Space Administration, sponsoring body.
Description
1 online resource (79 pages) : illustrations.
Series Statement
NASA TM ; X-73118
Uniform Title
NASA technical memorandum ; X-73118.
Subject
  • Supersonic inlets
  • Aerodynamics
  • Mach number
  • Jet engines > Air intakes
  • Airplanes > Air ducts
  • Air ducts > Aerodynamics
Note
  • "May 1976."
  • Includes appendix.
Bibliography (note)
  • Includes bibliographical references (page 22).
Type of Report (note)
  • Technical memorandum.
Funding (note)
  • NASA-Ames Research Center
Source of Description (note)
  • Description based on online resource; title from PDF title page (NASA, viewed on Oct. 26, 2021).
Call Number
GPO Internet NAS 1.15:X-73118
OCLC
marcive777159342
Author
Latham, Eldon A., author.
Title
Investigation of two bifurcated-duct inlet systems from Mach 0 to 2.0 over a wide range of angles of attack / Eldon A. Latham.
Publisher
Moffett Field, California : Ames Research Center, May 1976.
Type of Content
text
Type of Medium
computer
Type of Carrier
online resource
Series
NASA TM ; X-73118
NASA technical memorandum ; X-73118.
Bibliography
Includes bibliographical references (page 22).
Type Of Report
Technical memorandum.
Funding
NASA-Ames Research Center 5C5-04-11
Connect to:
https://purl.fdlp.gov/GPO/gpo171204
Added Author
Ames Research Center, issuing body.
United States. National Aeronautics and Space Administration, sponsoring body.
Other Form:
Print version: Latham, Eldon A Investigation of two bifurcated-duct inlet systems from Mach 0 to 2.0 over a wide range of angles of attack (OCoLC)92811674
Gpo Item No.
0830-D (online)
Sudoc No.
NAS 1.15:X-73118
View in Legacy Catalog