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Investigation Of Escape Capsule Systems For Multi-place Aircraft . Part I: Preliminary Investigation
Author(s): Vorachek, J. J. , Milhoan, F.Corporate Author(s): Goodyear Aircraft Corporation
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1961-12
Report number: WADC TR 57-329 Part 1
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Investigation Of Escape Capsule Systems For Multi-place Aircraft. Part II: Preliminary Design And wind Tunnel Testing Of An Individual Escape Capsule
Author(s): Milhoan, F. M., Vorachek, J. J., D'Allura, J.Corporate Author(s): Goodyear Aircraft Corporation
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1961-12
Report number: WADC TR 57-329 Part 2
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Automatic Runway Profile Measuring Instrumentation And Runway Properties. Part I: Equipment
Author(s): Turner, D. F., Brown, R. S., Snyder, W. E.Corporate Author(s): Midwest Research Institute
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1961-02
Report number: WADD TR 60-470 Part I
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Theoretical And Experimental Studies On Airloads Related To Hypersonic Aeroelastic Problems Of General Slender Pointed Configurations
Author(s): Zartarian, Garabed, Tan Hsu, PaoCorporate Author(s): Massachusetts Institute of Technology
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1961-04
Report number: ASD TR 61-7
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Structural Response Of Beryllium Sheet Produced By Three Fabrication Methods
Author(s): Giemza, C. J.Corporate Author(s): Martin Co Baltimore Md
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1961-12
Report number: ASD TR 61-87
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Compressible Boundary Layer Equations And Stagnation Point Solution With Differences In Thermal And Dynamic Boundary Layer Thicknesses Being Considered
Author(s): Buck, Melving L.Corporate Author(s): Aeronautical Systems Div Wright-Patterson AFB Ohio Flight Control Lab
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1961-08
Report number: ASD TR 61-107
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Feasibility To Determine Practicability Of Providing Mockup Improvements
Author(s): Lowe, W. F., Calvin, C. C., Doughty, L. E.Corporate Author(s): Chance Vought Aircraft, Incorporated
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1961-08
Report number: WADD TR 60-579
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Admittance Techniques In high Speed Flutter Model Testing. Part I. Experimental Results
Author(s): Asher, Gifford W., Watanabe, Roy K.Corporate Author(s): Boeing Company
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1961-07
Report number: WADD TR 61-31 Part I
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Automatic Runway Profile Measuring Instrumentation And Runway Properties. Part II: Equipment Trials
Author(s): Turner, D. F., Brown, R. S., Patton, P. C.Corporate Author(s): Midwest Research Institute
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1961-10
Report number: WADD TR 60-470 Part II
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- 1961 (9)
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- Brown, R. S. (2)
- Turner, D. F. (2)
- Asher, Gifford W. (1)
- Buck, Melving L. (1)
- Calvin, C. C. (1)
- D'Allura, J. (1)
- Doughty, L. E. (1)
- Giemza, C. J. (1)
- Lowe, W. F. (1)
- Milhoan, F. (1)
- Milhoan, F. M. (1)
- Patton, P. C. (1)
- Snyder, W. E. (1)
- Tan Hsu, Pao (1)
- Vorachek, J. J. (1)
- Vorachek, J. J. (1)
- Watanabe, Roy K. (1)
- Zartarian, Garabed (1)
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- Goodyear Aircraft Corporation (2)
- Midwest Research Institute (2)
- Aeronautical Systems Div Wright-Patterson AFB Ohio Flight Control Lab (1)
- Boeing Company (1)
- Chance Vought Aircraft, Incorporated (1)
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