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![AFFDLTR64-174.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/d721bef1c3be61914c70f8a284ee2e4969dbf421.jpg)
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An Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Kaufman, Louis G., II, Meckler, Lawrence, Hartofilis, Stavros A., Weiss, DanielCorporate Author(s): Grumman Aircraft Engineerign Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-01
Report number: AFFDL TR 64-174
![FDLTDR64-002part01.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/0dd3e036617f5ed1149c35edcff8f714b9f75655.jpg)
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Pressure and Heat Transfer Measurements for Mach 8 Flows Over a Blunt Pyramidal Configuration with Aerodynamic Controls: Part I: Pressure Data for Delta Wing Surface
Author(s): Kaufman, Louis G., IICorporate Author(s): Grumman Aircraft Engineerign Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-01
Report number: FDL TDR 64-2 Part 1
![FDLTDR64-002part03.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/e98c5604c0512f65c8d499d5b1ffac77ee186081.jpg)
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Pressure and Heat Transfer Measurements for Mach 8 Flows Over a Blunt Pyramidal Configuration with Aerodynamic Controls: Part III: Heat Transfer Data for Delta Wing Surface
Author(s): Kaufman, Louis G., IICorporate Author(s): Grumman Aircraft Engineerign Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-05
Report number: FDL TDR 64-2 Part 3
![FDLTDR64-002part04.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/9a9aaedfbeed81b39ab4f8b83f84b0dba990bb6c.jpg)
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Pressure and Heat Transfer Measurements for Mach 8 Flows Over a Blunt Pyramidal Configuration with Aerodynamic Controls: Part IV: Heat Transfer 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 Engineerign Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-05
Report number: FDL TDR 64-2 Part 4
![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
![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
![AFFDLTR72-066.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/2756fdde8b8df7da31df17119e847d0bdcee14ce.jpg)
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Interference Heating Due to Shock Impingement
Author(s): Haslett, Robert A., Romanowski, Richard F., Urkowitz, Michael, Kaufman, Louis G., IICorporate Author(s): Grumman Aerospace Corp Bethpage N Y
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1972-07
Report number: AFFDL TR 72-66
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