Search

list

11 items

application/pdf thumbnail
full text available
Aerodynamic Noise And The Estimation Of Noise In Aircraft
Author(s): Rogers, Orville R., Cook, Robert F.
Corporate Author(s): Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1952-02
Report number: WADC TR 52-341
full text unavailable
Wind Tunnel Tests of the Coanda Wing and Nozzle
Author(s): Young, D. W., Zonars, D.
Corporate Author(s): Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1950-09
Report number: AF TR 6199
full text unavailable
Rolling Effectiveness and Aileron Reversal Characteristics of Straight and Sweptback Wings: Part 3. Evaluation and Test Results
Author(s): Groth, Eric
Corporate Author(s): Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1952-09
Report number: AF TR 6198 Part 3
full text unavailable
Measurements with Honeycombs in the Full-Scale and in the Model Vertical Wind Tunnel
Author(s): Knackstedt, Wilhelm F.
Corporate Author(s): Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1952-08
Report number: WADC TR 52-207
application/pdf thumbnail
full text available
New Standard Atmosphere: The WADC 1952 Model Atmosphere
Author(s): Williams, D. T., Nash, W. F., Bell, J. C.
Corporate Author(s): Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1954-03
Report number: WADC TR 54-215
full text unavailable
Method For Predicting Dynamic Landing Loads
Author(s): Eisenman, Richard L., Kramer, Edward H.
Corporate Author(s): Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1954-09
Report number: WADC TR 54-28
full text unavailable
The Wall Pressure Distribution In A Choked Tunnel
Author(s): Guderley, Gottfried
Corporate Author(s): Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1953-12
Report number: WADC TR 53-509
full text unavailable
Subsonic Flutter Tests of an Unswept All-Movable Horizontal Tail
Author(s): Hoffman, Niles R., Spielberg, Irvin N.
Corporate Author(s): Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1954-03
Report number: WADC TR 54-53
application/pdf thumbnail
full text available
The Effect of an Axially Symmetric Fuselage on the Nonstationary Supersonic Airloads Acting on a Wing with Supersonic Edges
Author(s): Epstein, Melvin
Corporate Author(s): Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1954-05
Report number: WADC TR 54-196
full text unavailable
On The Flow Over A Finite Wedge In The Lower Transonic Region
Author(s): Yoshihara, Hideo
Corporate Author(s): Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1956-06
Report number: WADC TR 56-444

Refine your search

Refine your search