Blank Cover Image

A Parameter Study and Comparison of Projectiles with Fins and Flares at Hypervelocities

著者名:
Silton, S. ( U.S. Army Research Laboratory, Aberdeen Proving Ground, MD )  
掲載資料名:
AIAA meeting papers on disc
シリーズ名:
AIAA Paper : AIAA Applied Aerodynamics Conference
シリーズ巻号:
23rd
発行年:
2005
通号:
2005-4969
ペーパー番号:
AIAA Paper 2005-4969
出版情報:
[Reston, Va.]: American Institute of Aeronautics and Astronautics
ISSN:
10877215
言語:
英語
請求記号:
A07400/200511 [CD-ROM 2005 Disc 11]
資料種別:
テクニカルペーパー

類似資料:

1 テクニカルペーパー Comparison of Predicted Actuator Performance for Guidance of Supersonic Projectiles to Measured Range Data

Silton, S.

American Institute of Aeronautics and Astronautics
7 テクニカルペーパー Optimized Guidance of a Supersonic Projectile Using Pin Based Actuators

Massey, K., Guthrie, K., Silton, S.

American Institute of Aeronautics and Astronautics
2 テクニカルペーパー Testing the Maneuvering Performance of a Mach 4 Projectile

K. Massey, S. Silton

American Institute of Aeronautics and Astronautics
8 テクニカルペーパー Design Study Comparison of Plain Finned Versus Louvered Finned-Tube Condenser Heat Exchangers.

Stewart, S.W., Shelton, S.V.

American Society of Mechanical Engineers
3 テクニカルペーパー Base Drag Considerations on a 0.50-caliber Spinning Projectile

S. Silton, S. Dinavahi

American Institute of Aeronautics and Astronautics
9 テクニカルペーパー Wind Tunnel Study of a Fin Stabilized Guided Projectile

W. Blake, T. Cunningham

American Institute of Aeronautics and Astronautics
4 テクニカルペーパー Experimental Determination of the Effect of Rifling Grooves on the Aerodynamics of Small Caliber Projectiles

S. Silton, D. Webb

American Institute of Aeronautics and Astronautics
10 テクニカルペーパー CFD Investigation of Fin Aeroheating on a Hypersonic Projectile

Mcllwain, S., Chen, S., Khalid, M.

American Institute of Aeronautics and Astronautics
5 テクニカルペーパー Aerodynamic Jump at Hypervelocity

Plostins, P., Silton, S., Schmidt, E., Soencksen, K.

American Institute of Aeronautics and Astronautics
11 テクニカルペーパー Comparison of Computed and Measured Flight Characteristics of Fin Stabilized Projectiles

Dillon Jr.,R.E.

American Institute of Aeronautics and Astronautics
6 テクニカルペーパー Navier-Stokes Computations for a Spinning Projectile from Subsonic to Supersonic Speeds

Silton, S., Laboratory, U.S. Army Research

American Institute of Aeronautics and Astronautics
12 テクニカルペーパー NUMERICAL STUDY OF TWO -STAGE LIGHT-GAS HYPERVELOCITY PROJECTILE LAUNCHERS

Groth, C. P.T. et al.

National Aeronautics and Space Administration
1
 
2
 
3
 
4
 
5
 
6
 
7
 
8
 
9
 
10
 
11
 
12