NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

The auto‑search feature has been disabled based on user feedback. Enter a search term/phrase and click “Search” to begin.

Back to Results
Wind Tunnel Tests of an Inflatable AirplaneIn this video a wind tunnel investigation of aerodynamic and structural deflection characteristics of an inflatable airplane is shown. The film includes scenarios during wind tunnel tests of an inflatable airplane in the Langley Full Scale Tunnel with the main objective of obtaining load factors prior to wing buckle of 4.5 to 5.0 g. The inflation pressure during the test was indicated to be 7.0 psi.
Document ID
19970005033
Acquisition Source
Johnson Space Center
Document Type
Video
Date Acquired
August 17, 2013
Publication Date
October 9, 1996
Subject Category
Aerodynamics
Report/Patent Number
NONP-NASA-VT-97-1997005936
NASA-TM-111830
L-1642
Report Number: NONP-NASA-VT-97-1997005936
Report Number: NASA-TM-111830
Report Number: L-1642
Accession Number
97N13020
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Available Downloads

There are no available downloads for this record.

Related Records

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