Suggested Topics within your search.
Suggested Topics within your search.
- Fighter planes
- Airplanes 100
- Procurement 74
- Airplanes, Military 42
- Charts, diagrams, etc 41
- Design and construction 39
- Appropriations and expenditures 33
- Flight testing 32
- Finance 31
- Costs 30
- History 30
- Armed Forces 28
- Wind tunnel testing 27
- F-35 (Military aircraft) 25
- Wings 24
- Jet planes, Military 21
- Handling characteristics 20
- Stability of airplanes 20
- Testing 19
- Control 18
- Tail surfaces 18
- Aviation 17
- Evaluation 17
- Models 17
- F-22 (Jet fighter plane) 16
- Piloting 15
- Purchasing 15
- Aeronautics, Military 14
- Motors 14
- Aerodynamics 13
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Flight evaluation of a simplified gross thrust calculation technique using an F100 turbofan engine in an F-15 airplane /
Published 1981Online Access
Online Access
Government Document eBook -
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Wind-tunnel investigation of the contribution of a vertical tail to the directional stability of a fighter-type airplane /
Published 1952Government Document Book -
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The effect of rate of change of angle of attack on the maximum lift of a small model /
Published 1950Government Document Book -
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A flight determination of the tolerable range of effective dihedral on a conventional fighter airplane /
Published 1949Search for the full-text version of this title in HathiTrust
Government Document Book -
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Proposed retirement of A-10 aircraft : background in brief /
Published 2019Online Access
Government Document Website -
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Tactical aircraft modernization : issues for Congress /
Published 2018Online Access
Government Document Website -
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A comparison of wing loads measured in flight on a fighter-type airplane by strain-gage and pressure-distribution methods /
Published 1949Government Document Book -
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Aerodynamic parameters of an advanced fighter aircraft estimated from flight data preliminary results /
Published 1989Online Access
Online Access
Government Document Electronic eBook -
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Aerodynamic parameters of an advanced fighter aircraft estimated from flight data preliminary results /
Published 1989Connect to online resource
Government Document Microfilm Book -
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The effect of rate of change of angle of attack on the maximum lift coefficient of a pursuit airplane /
Published 1951Government Document Book -
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Analytical study of modification to the autopilot of a fighter airplane in order to reduce the response to side gusts /
Published 1956Government Document Book -
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Post-World War II fighters, 1945-1973 /
Published 1986Full Text (via Internet Archive)
Government Document eBook -
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