| DEMONSTRATION OF TWO-POINT FOCUSED LASER DIFFERENTIAL INTERFEROMETRY (2PFLDI) IN A MACH 18 FLOW
|
2021 |
Ceruzzi, Andrew |
| BALANCE CALIBRATION ANALYSIS BY SEQUENTIAL REGRESSION
|
2021 |
Kammeyer, Mark E. |
| ICE SHEAR ADHESION TEST METHODS REVIEW AND NEW IN SITU TEST METHOD
|
2021 |
Tetteh, Edem Y. |
| FLOW NON-UNIFORMITIES BEHIND ACCELERATING SHOCKWAVES IN SHOCK TUBES
|
2021 |
Satchell, Matthew |
| INFRARED THERMOGRAPHY ON A BICONIC MODEL IN HYPERSONIC EXPANSION TUBE FLOWS
|
2021 |
Cullen, Timothy G. |
| SYNERGISTIC NUMERICAL AND EXPERIMENTAL INVESTIGATIONS OF THE DYNAMIC STABILITY OF A RE-ENTRY LIFTING CAPSULE
|
2021 |
Nagai, Shinji |
| AERODYNAMIC CHARACTERISTICS OF TURBOJAV MEASURED WITH 1-M MAGNETIC SUSPENSION AND BALANCE SYSTEM
|
2021 |
Okuizumi, Hiroyuki |
| A DIGITAL ONE DEGREE OF FREEDOM MODEL OF AN ELECTROMAGNETIC POSITION SENSOR
|
2021 |
Weinmann, Michelle E. |
| DETERMINATION OF HYPERVELOCITY FREESTREAM CONDITIONS FOR A VIBRATIONALLY FROZEN NITROGEN FLOW
|
2021 |
Korte, John |
| INITIAL CALIBRATION OF THE MACH 18 CAPABILITY AT THE AEDC HYPERVELOCITY WIND TUNNEL NO. 9
|
2021 |
Lafferty, John F. |
| APPLICATION OF THE CONCEPTS OF LOAD STATE, LOAD SPACE, AND OUTPUT SPACE TO STRAIN-GAGE BALANCES
|
2021 |
Ulbrich, Norbert M. |
| COMPARISON OF TWO CALIBRATIONS OF NASA'S MC60 FIVE-COMPONENT SEMI-SPAN BALANCE
|
2021 |
Ulbrich, Norbert M. |
| DEVELOPMENT OF A DIRECT-CONNECT TESTING CAPABILITY IN THE HYPERTERP SHOCK TUNNEL
|
2021 |
Pee, Xiu Yi |
| VALIDATION OF SUB-MILLIMETER RESOLUTION PRESSURE MEASUREMENT ON FREE FLIGHT MODEL MACH 1.5
|
2021 |
Gonzales, Joseph |
| LIFT INTERFERENCE EFFECTS EVALUATION FOR POWERED MODELS IN CLOSED-WALL LOW-SPEED WIND TUNNELS
|
2021 |
Philipsen, Iwan |
| MODEL PREPARATION AREAS FOR PROPULSION AIRFRAME INTEGRATION TESTING AT THE NASA LANGLEY RESEARCH CENTER
|
2021 |
Jones, Gregory S. |
| SOME FUNDAMENTALS OF AEROPROPULSION FORCE ACCOUNTING
|
2021 |
Beale, David K. |
| DESIGN OF THE UNIVERSITY OF TENNESSEE HIGH-ENTHALPY TUNNEL
|
2021 |
Byrd, Andrew J. |
| DESIGN AND CHARACTERIZATION OF MACH 5 FLOW FOR HIGHLY TURBULENT HYPERSONIC TEST FACILITY
|
2021 |
Thornton, Mason R. |
| DEVELOPMENT OF THE NASA 10% HIGH-LIFT COMMON RESEARCH MODEL (CRM-HL)
|
2021 |
Fell, Jared |
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