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7 items
![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
![FDLTDR64-128.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/415f7b485af6e9dfae6f5094b83faa14bb6a174e.jpg)
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Aerodynamic Characteristics and Flap Loads for a Blunt Pyramidal Configuration at Mach 5 and 8: :Part of an Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Evans, William J., Kaufman, Louis G., IICorporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-09
Report number: FDL TDR 64-128
![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
![FDLTDR64-142.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
![FDLTDR64-144.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/96968103841a2b961b43a0272f14437108e67ed3.jpg)
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Pressure and Heat Transfer Measurements at Mach 13 and 19 for Flows Ahead of Ramps, Over Expansion Corners, and Past Fin-Plate Combinations: Part of an Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Hatofilis, Stavros A.Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-09
Report number: FDL TDR 64-144
![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
![FDLTDR64-002part02.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/d265dfcc831966b4fedd9782abb25de8c269f3a8.jpg)
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Pressure and Heat Transfer Measurements for Mach 8 Flows Over a Blunt Pyramidal Configuration with Aerodynamic Controls: Part II" Pressure Data for Dihedral Surfaces Part of an Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Kaufman, Louis G., IICorporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-09
Report number: FDL TDR 64-2 Part 2
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