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Format-Fortran Matrix Abstraction Technique. Volume V - Supplement I. Engineering User and Technical Report - Extended.
Author(s): Pickard, J.
Corporate Author(s): Douglas Aircraft Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1970-08
Report number: AFFDL TR 66-207 Volume V Supplement I
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Aircraft Motion Analysis
Author(s): Thelander, J. A.
Corporate Author(s): Douglas Aircraft Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-03
Report number: FDL TDR 64-70
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Methods for Predicting the Aerodynamic and Stability and Control Characteristics of STOL Aircraft: Volume III Engineering Methods
Author(s): Goldhammer, M. I., Lopez, M. L.
Corporate Author(s): Douglas Aircraft Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1973-12
Report number: AFFDL TR 73-146 Volume 3
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Methods for Predicting the Aerodynamic and Stability and Control Characteristics of STOL Aircraft: Volume II STOL Aerodynamic Methods Computer Program
Author(s): Goldhammer, M. I., Wasson, N. F.
Corporate Author(s): Douglas Aircraft Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1973-12
Report number: AFFDL TR 73-146 Volume 2
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Methods for Predicting the Aerodynamic and Stability and Control Characteristics of STOL Aircraft. Volume I. Basic Theoretical Methods.
Author(s): Goldhammer, M. I., Shen, C. C., Lopez, M. L.
Corporate Author(s): Douglas Aircraft Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1973-12
Report number: AFFDL TR 73-146 VOL. I
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Format-Fortran Matrix Abstraction Technique: Volume VI - Supplement II: Description of Digital Computer Program- Phase I - Extended
Author(s): Morris, R. C.
Corporate Author(s): Douglas Aircraft Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1973-04
Report number: AFFDL TR 66-207 Volume VI Supplement II
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Format-Fortran Matrix Abstraction Technique: Volume V Supplement II: Engineering User and Technical Report-Extended
Author(s): Pickard, J.
Corporate Author(s): Douglas Aircraft Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1973-04
Report number: AFFDL TR 66-207 Volume V Supplement II

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