NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
A critical evaluation of analytic methods for predicting laminar-boundary-layer shock-wave interactionPrediction methods for boundary layer and flow field characteristics in shock wave-boundary layer interaction
Document ID
19700012067
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Murphy, J. D. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 5, 2013
Publication Date
January 1, 1970
Publication Information
Publication: L. METHODS IN AIRCRAFT AERODYN. 1970
Subject Category
Aerodynamics
Accession Number
70N21372
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Document Inquiry

Available Downloads

There are no available downloads for this record.

Related Records

IDRelationTitle19700012046Collected WorksAnalytic Methods in Aircraft AerodynamicsN70-21351 09-01Collected Works
No Preview Available