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![FDLTDR64-007.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/7e275e7f2d222d545d8b6bfe5cd193c99ad32647.jpg)
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The Calculation of Nonlinear Supersonice Conical Flows by the Method of Integral Relations
Author(s): Brook, John W.Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-07
Report number: FDL TDR 64-7
![FDLTDR64-120.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/e2f97563261c3377ff91085a130db63b7ebd0077.jpg)
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Pressure and Heat Transfer Measurements fro Mach 21 Flows Over a Blunt Pyramidal Configuration with Aerodynamic Controls
Author(s): Kaufman, Louis G., IICorporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-08
Report number: FDL TDR 64-120
![FDLTDR64-124.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/69a5f060718a68abae188670a0eca41ea12ef330.jpg)
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Pressure Measurements at Mach 8 on an Aerodynamically Controllable Winged Re-Entry Configuration: Part of an Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Meckler, LawrenceCorporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1965-06
Report number: FDL TDR 64-124
![FDLTDR64-142.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/c2d9448d1bacdaaff536bdccde11aec4552b4694.jpg)
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Heat Transfer Measurements at Mach 9 on an Aerodynamically Controllable Winged Re-Entry Configuration: Part of an Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Meckler, LawrenceCorporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-09
Report number: FDL TDR 64-142
![RTDTDR63-4044part03.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/f186fe454b7ad3b01fb8222af483ca7fe32ac304.jpg)
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Pressure Measurements for Mach 8 Flows Over Expansion Corners and Ramps on an Internally Cooled Model Part III. Flows Over Full Span Ramps Mounted on a Flat Plate
Author(s): Kaufman, Louis G., IICorporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-05
Report number: RTD TDR 63-4044 Part 3
![FDLTDR64-010.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/9b381f18ecd0bc9349d091807eefecc1e718f0e6.jpg)
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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, LawrenceCorporate 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 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 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
Investigation of Dynamic Stability Derivatives of Vehicles Flying at Hypersonic Velocity
Author(s): Gilmore, Arthur, Seredinsky, Vladimir, MacKenzie, DonaldCorporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-09
Report number: ASD TDR 62-460
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