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
Advances in hypersonic extrapolation capability - Wind tunnel to flightHypersonic cruise aircraft configuration reliable Reynolds numbers extrapolation from laminar boundary to turbulent layer
Document ID
19710037879
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Penland, J. A.
Romeo, D. J.
Date Acquired
August 6, 2013
Publication Date
January 1, 1971
Publication Information
Publisher: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS,
Subject Category
Fluid Mechanics
Report/Patent Number
AIAA PAPER 71-132
Report Number: AIAA PAPER 71-132
Meeting Information
Meeting: AEROSPACE SCIENCES MEETING
Location: NEW YORK, NY
Start Date: January 25, 1971
End Date: January 27, 1971
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
71A18576
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