A simulated separation test of a tactical fighter dispenser munition from an F-105D parent aircraft was conducted using a captive trajectory system. Test variables included Mach number and launch conditions. (Author)
Separation Test of the 1/22 Scale Tfd from the F-105D Aircraft at the General Dynamics High Speed Wind Tunnel
1967
147 pages
Report
Keine Angabe
Englisch
Aircraft , Fluid Mechanics , Computer Hardware , Jet fighters , External stores , Separation , Airplane models , Supersonic characteristics , Transonic characteristics , Simulation , Wind tunnel models , Model tests , Scale , Computer programming , Firing tests(Ordnance) , Data processing , Analog computers , Digital systems , Test facilities , Test methods , Aerodynamic configurations , F-105 aircraft , F-105d aircraft
The continuing evolution of the Military Standard 105D sampling system
Tema Archiv | 1982
|High speed wind tunnel tests of the PTA aircraft
NTRS | 1986
|