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A Closed-Form Solution to Lifting Reentry
Author(s): Bell, Roland N.Corporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1966-01
Report number: AFFDL TR 65-65
full text available
General Instability of Orthotropically Stiffened Cylinders. Part 1. Axial Compression, Torsion and Hdyrostatic Pressure Loadings
Author(s): Milligan, Roger, Gerard, George, Lakshmikantham, C., Becker, HerbertCorporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-07
Report number: AFFDL TR 65-161 Part 1
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General Instability of Orthotropically Stiffened Cylinders. Part 2. Bending and Combined Compression and Bending.
Author(s): Lakshmikantham, C., Gerard, George, Milligan, RogerCorporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-08
Report number: AFFDL TR 65-161 Part 2
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The Effect Of Plastic Deformation On The Strain Energy Release Rate In A Centrally Notched Plate Subjected To Uniaxial Tension
Author(s): Forman, Royce G.Corporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1966-01
Report number: AFFDL TR 65-186
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Measurement And Analyses Of The J57-P21 Noise Field
Author(s): Hermes, P. H., Smith, D. L.Corporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1966-10
Report number: AFFDL TR 66-147
full text available
Low Pressure Type Expandable Aircraft Tire Characteristics
Author(s): Wagner, Paul M.Corporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1967-03
Report number: AFFDL TR 66-170
full text available
Application Of The Subdomain (Biezeno-Koch) Method To Circular Plate Bending
Author(s): Adams, O. E., JrCorporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1967-06
Report number: AFFDL TR 66-215
full text available
A Prototype Peripheral Vision Aircraft Attitude Display
Author(s): Williamson, William R.Corporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1966-10
Report number: AFFDL TR 66-91
full text available
Effects of Manipulator Restraints on Human Operator Performance
Author(s): Magdaleno, R. E., McRuer, D. T.Corporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1966-12
Report number: AFFDL TR 66-72
full text available
Stiffness and Vibration Characteristics of Inflatable Delta Wing Models at Temperatures up to 650°F
Author(s): Pollock, Samuel J.Corporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1966-06
Report number: AFFDL TR 66-14
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