NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
An experimental investigation of hypersonic turbulent boundary layers in adverse pressure gradient.Hypersonic turbulent boundary layer in adverse pressure gradients studied for transition, measuring static/pitot pressure, stagnation temperature and heat transfer rates
Document ID
19680036496
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hoydysh, W. G.
Zakkay, V.
Date Acquired
August 4, 2013
Publication Date
January 1, 1968
Publication Information
Publisher: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS.
Subject Category
Fluid Mechanics
Report/Patent Number
AIAA PAPER 68-44
Report Number: AIAA PAPER 68-44
Meeting Information
Meeting: AEROSPACE SCIENCES MEETING
Location: NEW YORK, NY
Start Date: January 22, 1968
End Date: January 24, 1968
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
68A17468
Funding Number(s)
CONTRACT_GRANT: NGR-33-016-067
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.

Related Records

There are no records associated with this record.
No Preview Available