Resource Type
Collection
Technical Report Archive and Image Library
87
National Advisory Committee for Aeronautics Collection
67
Office of Scientific & Technical Information Technical Reports
17
Texas Attorney General Opinions
16
TRAIL Microcard Collection
13
Government Documents A to Z Digitization Project
1
Texas State Publications
1
USDA Farmers' Bulletins
1
Serial/Series Title
NACA Research Memorandums
34
NACA Technical Notes
23
United States Geological Survey Reports
7
Atomic Energy Commission Reports
6
HW (Series)
6
Hanford Works Reports
6
NACA Technical Memorandums
5
NACA Technical Reports
5
Trace elements investigations report
5
Trace elements memorandum report
2
6 More
Country
States
122 Matching Results
Results open in a new window/tab.
prev
Results:
121 - 122 of
122
Wind-Tunnel Investigation of a 0.6-Scale Model of Hughes MX-904 Tail Surface at Supersonic Speeds: Tail Attached to a Segment of the Foreshortened Body
"An investigation has been made of a partial-span model of the tail surface designed for use on the Hughes Falcon (MX-904) missile to determine the aerodynamic characteristics of the tail and elevator including elevator hinge moment. Data obtained at Mach numbers of 1.62 and 1.96 in the Langley 9- by 12-inch supersonic blowdown tunnel are presented for the condition where the tail was attached to a segment of the foreshortened body" (p. 1).
Date:
May 4, 1950
Creator:
Conner, D. William & Guy, Lawrence D.
Object Type:
Report
System:
The UNT Digital Library
Wing-dropping characteristics of some straight and swept wings at transonic speeds as determined with rocket-powered models
Report presenting data gathered on a lateral-trim change or wing dropping that involves a rapid change of lateral trim with Mach number, which has occurred on several rocket-powered models used in roll investigations at transonic speeds. The data in this report demonstrates that straight wings with airfoil sections 9 percent thick or greater are susceptible to wing dropping between Mach numbers of 0.9 and 1.0. Results for straight, sweptback, and delta wings are provided.
Date:
May 26, 1950
Creator:
Stone, David G.
Object Type:
Report
System:
The UNT Digital Library