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STOL Tactical Aircraft Investigation - Externally Blown Flap Volume V Flight Control Technology Part III Stability and Control Derivative Accuracy Requirements and Effects of Augmentation System Design
Author(s): Elsanker, W. K., Okomoto, V. H.
Corporate Author(s): Rockwell International Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1973-04
Report number: AFFDL TR 73-20 Volume 5 Part 3
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STOL Tactical Aircraft Investigation - Externally Blown Flap Volume V Flight Control Technology Part II Simulation Studies/Flight Control System Validation
Author(s): Campbell, J. E., Okomuto, V. H., Elsanker, W. K.
Corporate Author(s): Rockwell International Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1973-04
Report number: AFFDL TR 73-20 Volume 5 Part 2
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STOL Tactical Aircraft Investigation - Externally Blown Flap Volume V Flight Control Technology Part I. Control System Mechanization Trade Studies
Author(s): Phillips, R. W.
Corporate Author(s): Rockwell International Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1973-04
Report number: AFFDL TR 73-20 Volume 5 Part 1
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STOL Tactical Aircraft Investigation - Externally Blown Flap Volume III Performance Methods and Takeoff and Landing Rules
Author(s): Renselaer, D. J.
Corporate Author(s): Rockwell International Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1973-04
Report number: AFFDL TR 73-20 Volume 3
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STOL Tactical Aircraft Investigation - Externally Blown Flap Volume II Design Compendium
Author(s): Roe, M. H., Quam, R. A., et al., Renselaer, D. J.
Corporate Author(s): Rockwell International Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1973-04
Report number: AFFDL TR 73-20 Volume 2
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STOL Tactical Aircraft Investigation - Externally Blown Flap Volume I Configuration Definition Supplement I Aerodynamic Trades of Flap and Roll Control System
Author(s): Renselaer, D. J.
Corporate Author(s): Rockwell International Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1973-04
Report number: AFFDL TR 73-20 Volume 1 Supplement 1
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STOL Tactical Aircraft Investigation Volume VI Air Cushion Landing System Study
Author(s): Gardner, Lloyd H., Milns, Peter, Pizzichemi, Charles J.
Corporate Author(s): The Boeing Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1973-05
Report number: AFFDL TR 73-19 Volume 6
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STOL Tactical Aircraft Investigation Volume IV Analysis of Wind Tunnel Data: Vectored Thrust/Mechanical Flaps and Internally Blown Jet Flaps
Author(s): Monk, John R., Palmer, Patrick, Lee, Jerry E.
Corporate Author(s): The Boeing Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1973-05
Report number: AFFDL TR 73-19 Volume 4
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STOL Tactical Aircraft Investigation Volume III Takeoff and Landing Performance Ground Rules for Powered Lift STOL Transport Aircraft
Author(s): Davenport, Franklyn J., Van Heyningen, Vernon F., Rengstorff, Arnold E.
Corporate Author(s): The Boeing Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1973-05
Report number: AFFDL TR 73-19 Volume 3
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STOL Tactical Aircraft Investigation Volume II, Part II A Lifting Line Analysis Method for Jet-Flapped Wings
Author(s): Davenport, Franklyn J.
Corporate Author(s): The Boeing Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1973-06
Report number: AFFDL TR 73-19 Volume 2 Part 2

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