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D. A. Boxwell
Observed names:
Boxwell, D. A.,
Boxwell, Donald A.,
D.A. Boxwell,
DONALD BOXWELL,
Donald A. Boxwell,
Donald Boxwell
show all 6
Observed institutions:
Ames Research Center,
United States Department of the Army,
U.S. Army Aviation and Missile Command,
United States Army
OpenAlex ID:
A5064409244
Helicopter Model Rotor‐Blade Vortex Interaction Impulsive Noise: Scalability and Parametric Variations
1987
·
D. A. Boxwell
, F. H. Schmitz
, et al.
·
Journal of the American Helicopter Society
·
95
PDF
In-Flight Far-Field Measurement of Helicopter Impulsive Noise
1976
·
F. H. Schmitz
, D. A. Boxwell
·
Journal of the American Helicopter Society
·
60
Full-Scale Measurements of Blade-Vortex Interaction Noise
1982
·
D. A. Boxwell
, F. H. Schmitz
·
Journal of the American Helicopter Society
·
56
Hovering impulsive noise - Some measured and calculated results
1978
·
D. A. Boxwell
, Y. H. Yu
, et al.
·
NASA STI Repository (National Aeronautics and Space Administration)
·
34
PDF
The Prediction of Transonic Flows on Advancing Rotors
1984
·
C. Tung
, F.X. Caradonna
, et al.
·
Vertical Flight Society Forum
·
31
Model‐ to Full‐Scale Comparisons of Helicopter Blade‐Vortex Interaction Noise
1984
·
F. H. Schmitz
, D. A. Boxwell
, et al.
·
Journal of the American Helicopter Society
·
29
High-Speed Helicopter Impulsive Noise
1977
·
F. H. Schmitz
, D. A. Boxwell
, et al.
·
Journal of the American Helicopter Society
·
25
Prediction of blade-vortex interaction noise using measured blade pressures
1987
·
MAHENDRA JOSHI
, SANDY LIU
, et al.
·
Aeroacoustics Conference
·
17
A note on the general scaling of helicopter blade-vortex interaction noise
1982
·
Fredric H. Schmitz
, D. A. Boxwell
, et al.
·
Adaptive Hardware and Systems
·
14
Prediction Measurement of a Low-Frequency Harmonic Noise of Hovering Model Helicopter Rotor
2000
·
F. H. Schmitz
, H. R. Aggarwal
, et al.
·
Journal of Aircraft
·
9
Model rotor high-speed impulsive noise - Parametric variations and full-scale comparisons
1983
·
W. R. Splettstoesser
, Klaus J. Schultz
, et al.
·
7
A comparison of the acoustic and aerodynamic measurements of a model rotor tested in two anechoic wind tunnels
1986
·
Boxwell, D. A.
, Splettstoesser, W. R.
, et al.
·
NASA Technical Reports Server (NASA)
·
5
PDF
Experiment versus theory
1982
·
Fredric H. Schmitz
, Y. H. Yu
, et al.
·
NASA Technical Reports Server (NASA)
·
4
Model Helicopter Rotor Aerodynamics and Acoustics As Measured in Two Anechoic Wind Tunnels
2000
·
F. H. Schmitz
, D. A. Boxwell
, et al.
·
Journal of Aircraft
·
1
Design, Analysis, and Experiments on a 10-inch Ducted Rotor VTOL UAV
2005
·
P.B. Martin
, D.A. Boxwell
·
Vertical Flight Society Unmanned Rotorcraft Systems Specialists Meeting
Ten Years of Cooperative Helicopter Aeroacoustics Research in the DNW.
1990
·
H. Heller
, W. Splettstößer
, et al.
·
elib (German Aerospace Center)
Prediction and Measurement of Low Frequency Hovering Harmonic Noise of a Modern Helicopter Rotor
1989
·
Fredric H. Schmitz
, H. R. Aggarwal
, et al.
Prediction and Measurement of Low-Frequency Harmonic Noise of a Hovering Model Helicopter Rotor
1989
·
H. R. Aggarawal
, D. A. Boxwell
, et al.
·
Vertical Flight Society Forum
Predictions and Measurement of Blade-Vortex Interaction Noise
1987
·
M. C. Joshi
, D. A. Boxwell
, et al.
Model 360 Rotor Test at Dnw - Review of Performance and Blade Airload Data
1987
·
Leo Dadone
, Don Ekquist
, et al.
·
Vertical Flight Society Forum
Prediction of Blade-vortex Interaction Noise
1987
·
Mahendra C. Joshi
, Sandy R. Liu
, et al.
·
Vertical Flight Society Forum
Full Scale Measurements of Helicopter Blade-vortex Interaction Impulsive Noise
1980
·
D. A. Boxwell
, F. H. Schmitz
·
Vertical Flight Society Forum
Acoustically swept rotor. [helicopter noise reduction]
1979
·
Fredric H. Schmitz
, D. A. Boxwell
, et al.
In-Flight Far-Field Measurement of Helicopter Impulsive Noise
1976
·
F. H. Schmitz
, D. A. Boxwell
·
Vertical Flight Society Forum
High-Speed Helicopter Impulsive Noise
1976
·
C. R. Vause
, F. H. Schmitz
, et al.
·
Vertical Flight Society Forum
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Works count:
30
Citation count:
387
H-index:
9
I10-index:
9
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