NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Research achievements review. Volume 3 - Aerophysics research at MSFCAerodynamic effects on rocket and launch vehicle design, shock tunnel simulation, jet exhaust flow, wind velocity measurements, and human auditory response model
Document ID
19690023911
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Date Acquired
September 2, 2013
Publication Date
January 1, 1968
Subject Category
Space Vehicles
Report/Patent Number
REPT-4
NASA-TM-X-53799
Report Number: REPT-4
Report Number: NASA-TM-X-53799
Accession Number
69N33289
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

IDRelationTitle19690023912WorkRockets at large angles of attack19690023913WorkLudwieg tube pilot test and high Reynolds number test equipment19690023914WorkTheoretical analysis of the starting process in the Ludwieg tube19690023915WorkFlow characteristics of orifices for venting launch vehicle compartments19690023916WorkPlume flow field analysis for liquid propellant rocket engines19690023917WorkTechniques developed to determine aerodynamic coefficients for Apollo applications program vehicles in an orbital environment19690023919WorkPerceived sound19690023920WorkRadiative heat transfer from Saturn exhaust plumes19690023921WorkDevelopment of laser-Doppler gas velocity instrumentation19690023922WorkOptical cross-beam investigation of local sound generation in jets19690023912WorkRockets at large angles of attack19690023913WorkLudwieg tube pilot test and high Reynolds number test equipment19690023914WorkTheoretical analysis of the starting process in the Ludwieg tube19690023915WorkFlow characteristics of orifices for venting launch vehicle compartments19690023916WorkPlume flow field analysis for liquid propellant rocket engines19690023917WorkTechniques developed to determine aerodynamic coefficients for Apollo applications program vehicles in an orbital environment19690023919WorkPerceived sound19690023920WorkRadiative heat transfer from Saturn exhaust plumes19690023921WorkDevelopment of laser-Doppler gas velocity instrumentation19690023922WorkOptical cross-beam investigation of local sound generation in jets
No Preview Available