Nagamatsu, Henry T.
- Kendall, James Madison (1956) An Experimental Investigation of Leading Edge Shock Wave-Boundary Layer Interaction at Hypersonic Speeds; 10.7907/6XVK-B331
- Baldwin, Lawrence Cloyd (1955) Viscous Effects on Static Pressure Distribution for a Slender Cone at a Nominal Mach Number of 5.8; 10.7907/XNB2-P865
- Howard, Weston Morgan (1955) An Experimental Investigation of Pressure Gradients Due to Temperature Gradients in Small Diameter Tubes; 10.7907/SQF1-5002
- Korkegi, Robert Hani (1954) Transition Studies and Skin Friction Measurements on an Insulated Flat Plate at a Hypersonic Mach Number; 10.7907/X3B9-VW73
- Yoler, Yusuf Amon (1954) The Hypersonic Shock Tube; 10.7907/853G-K555
- Quiel, Norwald Richard (1954) Impact Pressure and Total Temperature Interpretation at Hypersonic Mach Numbers; 10.7907/SMHA-4160
- Mark, Richard Muin (1954) Laminar Boundary Layers on Slender Bodies of Revolution in Axial Flow; 10.7907/4H6Z-K569
- Graves, Jack Carl (1954) Impact Pressure and Total Temperature Interpretation at Hypersonic Mach Number; 10.7907/V04Q-TF29
- Harkins, William Douglas (1954) Base Pressure and Static Pressure for a Cone-Cylinder at a Nominal Mach Number of 5.8; 10.7907/P0K8-XG38
- Eimer, Manfred (1953) Direct Measurement of Laminar Skin Friction at Hypersonic Speeds; 10.7907/MK2E-1P76
- Mackay, Douglas Severance (1953) Boundary Layer Temperature Recovery Factor on a Cone at Nominal Mach Number Six; 10.7907/8DEC-WE68
- Stoolman, Leo (1953) Investigation of an Instability Phenomena Occurring in Supersonic Diffusors; 10.7907/EG52-8V58
- DeLauer, Richard Daniel (1953) Experimental Heat Transfer at Hypersonic Mach Number; 10.7907/59SJ-TR03
- Grey, Jerry (1952) The Effects of Air Condensation on Properties of Flow and their Measurement in Hypersonic Wind Tunnels; 10.7907/HFHE-HR77
- Buhler, Rolf Dietrich (1952) Condensation of Air Components in Hypersonic Wind Tunnels: Theoretical Calculations and Comparison with Experiment; 10.7907/0J8Q-9Z82
- Arthur, Paul David (1952) Effects of Impurities on the Supersaturation of Nitrogen in a Hypersonic Wind Tunnel; 10.7907/PBSD-2V70
- Scherer, Lee Richard (1950) Aerodynamic Characteristics of a Wedge and Cone at Hypersonic Mach Numbers; 10.7907/29PE-XX71
- Frick, Leo Francis (1950) Experimental Investigation of Detached Shock on a 70° Cone at Various Angles of Attack; 10.7907/D4TV-0W57
- Chase, Patrick Stanley (1950) Flexible Plate Supersonic Wind Tunnel Flow Correction to Account for Plate Elastic Properties; 10.7907/EC0T-P917
- DeLauer, Richard Daniel (1950) Aerodynamic Characteristics of a Wedge and Cone at Hypersonic Mach Numbers; 10.7907/rndh-4a17
- Barish, David Theodore (1950) Acoustical Airspeed Indicators; 10.7907/FR7P-K372
- Alperin, Morton (1950) A Study of Detached Shock Waves in Two-Dimensions; 10.7907/NW30-HY03
- Bryan, William Cleveland (1950) Experimental Investigation of Detached Shock on a 70° Cone at Various Angles of Attack; 10.7907/XAZW-8051
- Bacon, John William (1949) An Investigation of Blowing as a Method of Increasing the Maximum Lift of a Double-Wedge Airfoil; 10.7907/NT63-HE54
- Muirhead, Vincent Uriel (1949) Flow Field Around a Finite Cone with Shock; 10.7907/7GMA-0V07
- Shonerd, David Edwin (1949) Winged Rocket Performance Analysis; 10.7907/34ZH-KG02
- Blenkush, Philip George (1949) A Wind Tunnel Investigation of the Aerodynamic Characteristics of High-Lift Devices on Supersonic Wings at Low Subsonic Speed; 10.7907/N6XA-GR06
- Burke, James Donahue (1949) Sounding Rocket Performances Analysis; 10.7907/XW5Q-1Y06
- Densmore, James Edward (1949) Wind Tunnel Investigation of the Aerodynamic Characteristics of High Lift Devices on Supersonic Wings at Low Subsonic Speed; 10.7907/Z0Y9-J658
- Thomas, John William (1949) Low Speed Wind Tunnel Investigation of High Lift Devices on a 65° Swept-Back Supersonic Wing of 3.44 Aspect Ratio; 10.7907/TYRW-TZ93
- MacKinnon, Neil Allan (1949) Flow Field Around a Finite Cone with Shock; 10.7907/XR4M-9R51
- Marx, Michael Ferdinand (1949) Low Speed Wind Tunnel Investigation of High Lift Devices on a 65° Swept-Back Supersonic Wing of 3.44 Aspect Ratio; 10.7907/2B48-J790
- Marschner, Bernard Walter (1948) An Investigation of Detached Shock Waves
- Jensen, Arnold Axtell and Koerner, Warren Gottlieb (1948) Wind Tunnel Investigation of a Supersonic Tailless Airplane at Low Subsonic Speed; 10.7907/KFRK-AF65
- Altseimer, John H. (1948) An Experimental Investigation of Detached Shock Waves; 10.7907/W6SF-EG14
- Magnus, Richard Jeffrey (1948) Study of Vortex Shedding as Related to Torsional Oscillations of a Thin Airfoil; 10.7907/NAKT-DG24
- Chuan, Raymond Lu-Po (1948) An Investigation of Vortex Shedding as Related to the Self-Excited Torsional Oscillation of an Airfoil; 10.7907/6JQH-FS81
- Pollock, Albert David and Reck, Floyd Francis (1947) A Study of Methods to Increase the Lift of Supersonic Airfoils at Low Speeds; 10.7907/J3NG-DD26