Search

list

9 items

application/pdf thumbnail
full text available
Static Aerodynamic Characteristics at Mach 5 and 8 of an Aerodynamically Controllable Winged Re-Entry Configuration. Part of an Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Meckler, Lawrence
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-09
Report number: FDL TDR 64-10
full text by request
Pressure and Heat Transfer Measurements for Flows Ahead of Ramps Part III: Mach 8 Pressure Data for Flows Ahead of Ramps: Part of an Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Kaufman, Louis G.
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1963-12
Report number: ASD TDR 63-679 Part 3
full text by request
Pressure and Heat Transfer Measurements for Hypersonic Flows over Expansion Corners and Ahead of Ramps Part II: Mach 5 Pressure Data for Flows Ahead of Ramps: :Part of an Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Kaufman, Louis G.
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-09
Report number: ASD TDR 63-679 Part 2
full text unavailable
Pressure and Heat Transfer Measurements for Hypersonic Flows over Expansion Corners and Ahead of Ramps Part I: Mach 5 and 8 Data for Expansion Corner Flows: Part of an Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Kaufman, Louis G.
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-09
Report number: ASD TDR 63-679 Part 1
full text unavailable
Pressure Measurement at Mach 19 for a Winged Re-Entry Configuration: Part of an Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Hartofilis, Stavros A.
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: Flight Control Division
Date of Publication: 1963-05
Report number: ASD TDR 63-319
full text by request
Pressure Distributions and Oil Film Photographs for Mach 5 Flows Past Fins Mounted on a Flat Plate: Part of an Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Kaufman, Louis G.
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-09
Report number: ASD TDR 63-755
full text unavailable
Experimental Investigation of Pressures on a Blunt Two-Dimensional Profile and on Sharp and Blunt Conical Shapes of Noncircular Cross Section at Mach 5 and 8
Author(s): Mead, Harold R., Koch, Frank
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: Flight Control Laboratory
Date of Publication: 1963-08
Report number: ASD TDR 63-169
full text unavailable
Pressure and Heat Transfer Measurements at Mach 5 and 8 for a Fin-Flat Plate Model: Part of an Investigation of Hypersonice Flow Separation and Control Characteristics
Author(s): Kaufman, Louis G., Meckler, Lawrence
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: Flight Control Laboratory
Date of Publication: 1963-04
Report number: ASD TDR 63-235
full text unavailable
Investigation of Dynamic Stability Derivatives of Vehicles Flying at Hypersonic Velocity
Author(s): Gilmore, Arthur, Seredinsky, Vladimir, MacKenzie, Donald
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-09
Report number: ASD TDR 62-460

Refine your search

Refine your search