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Study of Folding Proprotor VTOL Aircraft Dynamics. Volume I. Analytical Methods.
Author(s): Yen, Jing G., Gaffey, Troy M., Weber, Gottfried E.Corporate Author(s): Bell Helicpter Textron Inc., Fort Worth, Texas
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1971-09
Report number: AFFDL TR 71-7 Volume 1
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Statistical Analysis of LO-LOCAT Turbulence Data for Use in the Development of Revised Gust Criteria
Author(s): McCloskey, John W., Ryan, John P., Engler, Nicholas A., Luers, James K.Corporate Author(s): Dayton University Research Institute
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1971-04
Report number: AFFDL TR 71-29
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Theory of an Air Cushion Landing System for Aircraft
Author(s): Digges, Kennerly H.Corporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1971-06
Report number: AFFDL TR 71-50
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Design Studies and Model Tests of the Stowed Tilt Rotor Concept. Volume II. Component Design Studies.
Author(s): Fry, Bernard L.Corporate Author(s): Boeing Vertol Company, Philadelphia, Pennsylvania
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1971-07
Report number: AFFDL TR 71-62 Volume 2
full text by request
New Techniques in Nondestructive Testing (Exo-Electron Emission Phase). Part I.
Date of Publication: 1971-12 Report number: AFML TR 71-140
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AFML Torsional Split Hopkinson Bar
Date of Publication: 1971-07 Report number: AFML TR 71-145
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Development of a High Speed Biaxial Testing Machine
Date of Publication: 1971-07 Report number: AFML TR 71-149
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Analytical Study of the Split Hopkinson Bar Technique for Strain-Rate Dependent Material Behavior
Date of Publication: 1971-08 Report number: AFML TR 71-155
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Development and Applications of Nondestructive Methods for Predicting Mechanical Properties of Advanced Reinforced Nonmetallic Composites.
Date of Publication: 1971-09 Report number: AFML TR 71-168
full text by request
Fine Subgrain Structure Adjacent to Fatigue Cracks
Date of Publication: 1971-10 Report number: AFML TR 71-211
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