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Unsteady Aerodynamics for Advanced Configurations: Part VII - Velocity Potentials in Non-Uniform Transonic Flow Over a Thin Wing
Author(s): Andrew, L. V., Stenton, T. E.
Corporate Author(s): North American Rockwell Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1968-08
Report number: FDL TDR 64-152 Part 7
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Format-Fortran Matrix Abstraction Technique. Volume VI. Description Of Digital Computer Program - Phase I.
Author(s): Cogan, J. P., Jr., Morris, R. C., Serpanos, J. E, Wells, J. R.
Corporate Author(s): McDonnell Douglas Corporation, Douglas Aircraft Division
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1968-12
Report number: AFFDL TR 66-207 Volume VI
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Format - Fortran Matrix Abstraction Technique. Volume V. Engineering User And Technical Report.
Author(s): Pickard, J.
Corporate Author(s): Douglas Aircraft Company, Aircraft Division
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1968-12
Report number: AFFDL TR 66-207 Volume V
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Format II - Second Version of Fortran Matrix Abstraction Technique: Volume II, Supplement I,: Description of Digital Computer Program
Author(s): Lackey, W. J., Wild, R. E.
Corporate Author(s): McDonnell Douglas Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1968-12
Report number: AFFDL TR 66-207 Volume 2 Supplement 1
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Design Criteris for the Predition and Prevention of Panel Flutter. Volume I: Criteria Presentation
Author(s): Lemley, Clark E.
Corporate Author(s): McDonnell Douglas Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1968-08
Report number: AFFDL TR 67-140
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Assessment Of The Factors Affecting Advanced Lifting Entry Vehicles
Author(s): Draper, Alfred C., Buck, Melvin L.
Corporate Author(s): Air Force Flight Dynamics Lab Wright-Patterson AFB OH
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1968-01
Report number: AFFDL TR 67-137
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Wind Tunnel Studies Of The Pressure Distribution And The Flow Field In The Wake Of The Lockheed C-141A Starlifter Jet Transport Aircraft
Author(s): Goodrick, T. F.
Corporate Author(s): Minnesota Univ Minneapolis Dept Of Aeronautics And Engineering Mechanics
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1968-05
Report number: AFFDL TR 67-163
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Prediction Of Boundary Layer Pressure Fluctuations
Author(s): Lowson, Martin V.
Corporate Author(s): Wyle Labs Inc Huntsville AL Testing Div
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1968-04
Report number: AFFDL TR 67-167
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Parametric Performance Analysis Of Crew Escape Concepts In The Vtol And Conventional Take-Off And Landing Situations
Author(s): Brown, Dean W., Standish, David B.
Corporate Author(s): North American Rockwell Corp Los Angeles CA Los Angeles Div
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1968-01
Report number: AFFDL TR 67-178
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Optimal Control Method For Predicting Control Characteristics And Display Requirements Of Manned-Vehicle Systems
Author(s): Elkind, Jerome I., Falb, Peter L., Kleinman, David, Levison, William H.
Corporate Author(s): Bolt Beranek And Newman Inc Cambridge Mass
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1968-06
Report number: AFFDL TR 67-187

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