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15 items
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Active Control Synthesis for Flexible Vehicles: Volume I. KONPACT Theoretical Description
Author(s): Konar, A. F., Stone, C. R., Hank, M., Mahesh, J. K.Corporate Author(s): Honeywell Systems & Research Center
Laboratory: U. S. Air Force Flight Dynamics Laboratory
Date of Publication: 1976-07
Report number: AFFDL TR 75-146 Volume 1
full text available
Active Control Synthesis for Flexible Vehicles: Volume II. KONPACT Program Listing
Author(s): Konar, A. F., Stone, C. R., Hank, M., Mahesh, J. K.Corporate Author(s): Honeywell Systems & Research Center
Laboratory: U. S. Air Force Flight Dynamics Laboratory
Date of Publication: 1976-07
Report number: AFFDL TR 75-146 Volume 2
full text available
Active Control Synthesis for Flexible Vehicles: Volume III. KONPACT User's Manual
Author(s): Konar, A. F., Stone, C. R., Hank, M., Mahesh, J. K.Corporate Author(s): Honeywell Systems & Research Center
Laboratory: U. S. Air Force Flight Dynamics Laboratory
Date of Publication: 1976-07
Report number: AFFDL TR 75-146 Volume 3
full text available
Vuilleumier Cooler Wear Rate Test Program
Author(s): Ohara, T., Gardos, M. N., Moore, K. G.Corporate Author(s): Hughes Aircraft Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1976-12
Report number: AFFDL TR 76-135
full text available
A Laboratory Investigation into Flight Perturbations During Steep Descents of V/STOL Aircraft
Author(s): Reid, L. D., Teunissen, H. W., Hughes, P. C., Etkin, B.Corporate Author(s): University of Toronto Institute for Aerospace Studies
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1976-08
Report number: AFFDL TR 76-84
full text available
Direct Side Force Control Criteria for Dive Bombing: Volume I - Summary
Author(s): Brulle, Robert V., Marsh, Richard G., Moran, William A.Corporate Author(s): McDonnell Aircraft Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1976-09
Report number: AFFDL TR 76-78 Volume 1
full text by request
An Investigation of Separated Flow About a Hemisphere-Cylinder at 0- to 19-Deg Incidence in the Mach Number Range from 0.6 to 1.5
Author(s): Hsieh, T.Corporate Author(s): ARO, Inc.
Laboratory: Propulsion and Wind Tunnel Facility
Date of Publication: 1976-11
Report number: AEDC TR 76-112
full text available
Space Shuttle
Corporate Author(s): National Aeronautics and Space AdministrationDate of Publication: 1976
Report number: NASA SP-407
full text by request
DYNALIST II. A Computer Program for Stability and Dynamic Response Analysis of Rail Vehicle Systems. Volume IV. Revised User's Manual
Author(s): Bronowicki, Allen, Hasselman, T. K.Corporate Author(s): J. H. Wiggins Company
Date of Publication: 1976-07
Report number: FRA-OR&D-75-22.IV
full text by request
DYNALIST II: A Computer Program for Stability and Dynamic Response Analysis of Rail Vehicle Systems: Volume III: Technical Report Addendum
Author(s): Bronowicki, Allen, Hasselman, T. K.Corporate Author(s): J. H. Wiggins Company
Date of Publication: 1976-07
Report number: FRA-OR&D-75.22.III
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- Hank, M. (3)
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