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William Saric

Research Activity: 
  • Saric,William S. Flow Quality Measurements in the NASA-Ames 11-Foot Unitary Plan Tunnel. NORTHROP GRUMMAN(12/7/2004 - 12/31/2004).
  • Saric,William S. Flight Experiments on Laminarization of Swept-Wing Boundary Layers Using Periodically Distributed Roughness Elements. UNIVERSAL TECHNOLOGY CORP(6/22/2004 - 1/22/2005).
  • Reed,Helen Louise*, Saric,William S. HIGH LIFT OVER DRAG ACTIVE (HILDA) WING. LOCKHEED MARTIN INC(1/21/2002 - 4/1/2004).
  • Saric,William S*, Reed,Helen Louise. DESIGN AND STABILITY CHARACTERISTICS OF A QSP AIRFOIL. LOCKHEED MARTIN INC(5/7/2001 - 12/31/2002).
  • Saric,William S*, Reed,Helen Louise. SUPERSONIC LAMINAR FLOW CONTROL ON SWEPT WINGS USING DISTRIBUTED ROUGHNESS. DOD-DARPA(12/1/2000 - 6/24/2004).
  • Lopez,Juan Manuel*, Saric,William S. SPATIAL & TEMPORAL RESONANCES IN HYDRODYNAMICS: A THEORETICAL, EXPERIMENTAL & NUMERICAL EXPLORATION. NSF-ENG(4/1/2000 - 3/31/2003).
  • Saric,William S*, Radeztsky,Ronald Henry. PULSED-SOUND MEASUREMENTS OF THE INFLUENCE OF HIGH-AMPLITUDE NOISE ON BOUNDARY-LAYER TRANSITION TO TURBULENCE. DOD-AFOSR(11/15/1999 - 11/14/2002).
  • Saric,William S*, Radeztsky,Ronald Henry. BOUNDARY-LAYER RECEPTIVITY MEASUREMENTS USING ACOUSTIC WAVE-PACKET FORCING. NSF-ENG(10/1/1999 - 9/30/2002).
  • Saric,William S. IUTAM SYMPOSIUM: LAMINAR-TURBULENT TRANSITION. NSF-ENG(9/15/1999 - 8/31/2000).
  • Saric,William S. IUTAM SYMPOSIUM: LAMINAR-TURBULENT TRANSITION. DOD-NAVY-ONR(8/1/1999 - 12/31/1999).
  • Saric,William S. LEADING-EDGE ROUGHNESS AS A TRANSITIONAL CONTROL MECHANISM. NORTHROP GRUMMAN(10/16/1998 - 4/15/1999).
  • Reed,Helen Louise*, Saric,William S. AERODYNAMIC STUDIES OF MICRO AIR VEHICLES. DOD-AIR FORCE(10/1/1998 - 9/30/2001).
  • Saric,William S. NATIONAL DEFENSE SCIENCE & ENGINEERING GRADUATE FELLOWSHIP PROGRAM. SCEEE SERVICES CORP(8/1/1998 - 8/31/2000).
  • Saric,William S*, Reed,Helen Louise. ACTIVE FLOW CONTROL ON HURLEY'S FREE-STREAMLINE AIRFOIL & DELTA WING. UNIV OF AZ(3/1/1998 - 8/31/1998).
  • Saric,William S. SCANNING LASER BIVROMETER FOR MEMS CONTROL DEVICES. DOD-AIR FORCE(1/1/1998 - 2/28/1999).
  • Saric,William S. CONTROL OF TRANSITION IN SWEPT-WING BOUNDARY LAYERS USING MEMS DEVICES AS DISTRIBUTED ROUGHNESS. DOD-AIR FORCE(7/15/1997 - 12/31/2000).
  • Saric,William S. SWEPT-WING RECEPTIVITY STUDIES USING DISTRIBUTED ROUGHNESS. NASA-LANGLEY RESEARCH CTR(6/1/1997 - 10/31/1999).
  • Saric,William S. EFFECTS OF SUCTION ON SWEPT-WING TRANSITION. BOEING AERO DIVISION-SEATTLE(5/19/1996 - 12/31/1996).
  • Saric,William S. INFLUENCE OF HIGH AMPLITUDE NOISE ON BOUNDARY LAYER TRANSITION TO TURBULENCE. DOD-AIR FORCE(5/1/1996 - 7/14/1998).
  • Saric,William S. SURGE CONTROL VALVE TEST. SCIENTIFIC MONITORING INC(5/1/1996 - 8/31/1996).
  • Saric,William S. Receptivity & Control of Boundary Layers Influenced by Body Forces. NATL RESEARCH COUNCIL(1/18/1996 - 12/31/1997).
  • Saric,William S. EFFECTS OF SUCTION OF SWEPT-WING TRANSITION. NASA-LANGLEY RESEARCH CTR(12/16/1995 - 3/31/1998).
  • Saric,William S. DYNAMIC CALIBRATION OF HOT-FILM SENSORS USING CONTROLLED INSTABILITY WAVES. CLARKSON UNIV(8/1/1994 - 7/31/1996).
  • Reed,Helen Louise*, Laananen,David Horton, Saric,William S. AERODYNAMICS OF THE ALRGE-VOLUME, FLOW-THROUGH DETECTOR. LANL(7/1/1994 - 9/30/1995).
  • Saric,William S. RECEPTIVITY IN BOUNDARY-LAYER TRANSITION TO TURBULENCE. DOD-AIR FORCE(10/15/1993 - 5/14/1996).
  • Saric,William S. HYBRID LAMINAR FLOW CNTL EXP IN THE NASA AMES. 11-FAST TUN. NASA(9/1/1992 - 3/31/1993).
  • Saric,William S. CONTROL OF UNSTABLE WAVES IN 3-DIMENSIONAL BOUNDARY LAYERS. NASA-LANGLEY RESEARCH CTR(2/23/1990 - 11/15/1995).
  • Saric,William S. EFFECT OF SOUND ON BOUNDARY-LAYER STABILITY. NASA(12/1/1989 - 12/31/1992).
  • Saric,William S. BOUNDARY LAYER STABILITY IN LAMINAR FLOW CONTROL. NASA(6/15/1989 - 12/31/1989).
  • Saric,William S. TRANSITION STUDIES ON A SWEPT WING MODEL. NASA-LANGLEY RESEARCH CTR(1/6/1989 - 5/15/1994).
  • Saric,William S. WIND TUNNEL TESTING. MOTOROLA, INC(10/9/1987 - 12/31/1987).
  • Saric,William S. BOUNDARY LAYER STABILITY ON A SWEPT WING. NASA-LANGLEY RESEARCH CTR(8/16/1987 - 4/15/1989).
  • Saric,William S. UNSTEADY LOW-REYNOLDS NUMBER AERODYNAMICS. DOD-NAVY(6/16/1985 - 5/15/1991).
  • Saric,William S. THREE DIMENSIONAL STRUCTURE OF TRANSITIONAL BOUNDARY LAYERS. DOD-AIR FORCE(6/15/1985 - 11/14/1989).