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Record Details

Record 48 of 17435
Transonic Wind-Tunnel Investigation of the Static Longitudinal Aerodynamic Characteristics of Several Configurations of the Scout Vehicle and of a Number of Related Models
Offline Availability: Go to Request Form
Author and Affiliation:
Kelly, Thomas C.(NASA Langley Research Center, Hampton, VA, United States)
Abstract: Results have been obtained i n t h e Langley 8-foot transonic pressure tunnel at Mach numbers from 0.40 t o 1.20 for several configurations of the Scout vehicle and f o r a number of related models. Tests extended over an angle-of-attack range from about -10 degrees to 10 degrees at a Reynolds number per foot of about 3.8 x 10 sup 6.
Publication Date: May 01, 1961
Document ID:
20040008085
(Acquired Jan 27, 2004)
Subject Category: AERODYNAMICS
Report/Patent Number: NASA-TN-D-794, L-1146
Document Type: Technical Report
Financial Sponsor: NASA; Washington, DC, United States
Organization Source: NASA Langley Research Center; Hampton, VA, United States
Description: 70p; In English
Distribution Limits: Unclassified; Publicly available; Unlimited
Rights: No Copyright
NASA Terms: AERODYNAMIC CHARACTERISTICS; ROCKET VEHICLES; ANGLE OF ATTACK; REYNOLDS NUMBER; WIND TUNNEL TESTS; AXIAL LOADS
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