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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
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
full text available
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
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
full text available
Fundamental Relationships for Ablation and Hyperthermal Heat Transfer
Author(s): Achard, Robert T.Corporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1966-04
Report number: AFFDL TR 66-25
full text available
Experimental Program to Determine Effect of Crack Buckling and Specimen Dimensions on Fracture Toughness of Thin Sheet Materials
Author(s): Forman, R. G.Corporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1966-01
Report number: AFFDL TR 65-146
full text available
Design and Performance of a 15 KW Wide Band Acoustic Facility
Author(s): Hankel, Keith M., Henderson, John P.Corporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1966-03
Report number: AFFDL TR 66-8
full text available
Opening Remarks
Author(s): Buck, George T.Corporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1966-11
Report number: AFFDL-TR-66-80 p. 1
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