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V/STOL wind-tunnel testing [microform] / David G. Koenig.
Microform
Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1984]
1984
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS95840Results of S5 CH tests with an ARL (Aerospace Research Laboratory) cascade [microform] / A. Fourmaux.
Microform
Washington, D.C. : National Aeronautics and Space Administration, [1984]
1984
0 resources
Fan blade shake test results for the 40- by 80-/80- by 120-foot wind tunnel [microform] / William Warmbrodt and Todd Graham.
Microform
Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1984]
1984
0 resources
New investigation of short wings with lateral jets [microform] / E. Carafoli and N. Camarasescu.
Microform
Washington, D.C. : National Aeronautics and Space Administration, [1983]
1983
0 resources
Effect of forebody strakes on the aerodynamic characteristics in pitch and sideslip of a hypersonic airplane configuration at Mach numbers of 1.41, 2.01, and 6.86 / by Cornelius Driver.
Web Resource
Washington : National Aeronautics and Space Administration, September 1959.
1959-9
1 resource
Available online
0A transonic wind-tunnel investigation of the static longitudinal and lateral aerodynamic characteristics of a proposed hypersonic glider with several booster configurations / by Ralph P. Bielat.
Web Resource
Washington : National Aeronautics and Space Administration, December 1960.
1960-12
1 resource
Available online
0Wind tunnel testing of high-rise buildings : an output of the CTBUH Wind Engineering Working Group / Peter Irwin, Roy Denoon & David Scott.
Book/Text
Milton Park, Abingdon, Oxon : Routledge, 2013.
2013
1 item
| Format | Call number | Item location |
|---|---|---|
| FormatBook/Text | Call numberTA654.5 .I78 2013 | Item locationOff-site |
Some low-speed problems of high-speed aircraft by A. Spence and D. Lean.
Book/Text
Paris, Advisory Group for Aeronautical Research and Development, 1961.
1961
1 item
| Format | Call number | Item location |
|---|---|---|
| FormatBook/Text | Call numberAGARD-R-357 | Item locationOff-site |
Verification of three-dimensional flutter calculations by means of wind-tunnel tests on a flexible model / by R. Destuynder and L. Darovsky (Office National d'Etudes et de Recherches Aerospatiales 29, Avenue de la Division Leclerc, 92 Châtillon, France).
Book/Text
Paris : Advisory Group for Aeronautical Research and Development, 1966.
1966
1 item
| Format | Call number | Item location |
|---|---|---|
| FormatBook/Text | Call numberAGARD-R-562 | Item locationOff-site |
Tunnel-wall effects associated with vtol-stol model testing by R.E. Kuhn and R.L. Naeseth.
Book/Text
Paris, Advisory Group for Aeronautical Research and Development, 1959.
1959
1 item
| Format | Call number | Item location |
|---|---|---|
| FormatBook/Text | Call numberAGARD-R-303 | Item locationOff-site |
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