WIND TUNNEL TESTS ON THE H3P78, POWER LAW, ELLIPTIC SECTION FLARED PROJECTILE FROM MACH 2.5 TO 4.0

WIND TUNNEL TESTS ON THE H3P78, POWER LAW, ELLIPTIC SECTION FLARED PROJECTILE FROM MACH 2.5 TO 4.0

Author(s):

Orchard,D.M. ( QinetiQ )
Fournier,E.Y. ( DREV )
Dupuis,A. ( DSTL )
Edwards,J.A.

Publication title:

AIAA paper

Title of ser.:

AIAA Paper : AIAA Atmospheric Flight Mechanics Conference

Ser. no.:

2001

Pub. Year:

2001

No.:

2001-4321

Paper no.:

AIAA-2001-4321

Page(from):

1

Page(to):

13

Pages:

13

Pub. info.:

Reston, VA: American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00050829
Series ID:	PA00000162
Conf. info. (Name):	AIAA Atmospheric Flight Mechanics Conference and Exhibit
Conf. info. (Number):	2001
Conf. info. (Venue):	Montreal, Quebec, Canada
Conf. info. (Date):	2001.08.06-2001.08.09
Note for article:	Atmospheric Flight Mechanics Conference and Exhibit 6th - 9th August 2001 Montreal, Canada

Similar Items:

1 Technical Paper WIND TUNNEL TESTS ON THE H3P78, POWER LAW, ELLIPTIC SECTION FLARED PROJECTILE WITH JET INTERACTION Orchard,D.M., Fournier,E.Y., Dupuis,A., Edwards,J.A. American Institute of Aeronautics and Astronautics	7 Technical Paper Wind Tunnel Investigation of Grid Fin and Conventional Planar Control Surfaces Fournier,E.Y. American Institute of Aeronautics and Astronautics
2 Technical Paper Base cavity effects on the aerodynamic characteristics of a hypersonic flared projectile Fournier, E.Y., Dupuis, A.D. American Institute of Aeronautics and Astronautics	8 Technical Paper Free-Flight Range Tests and Numerical Computations of a Power-Law Elliptic Cross-Section Projectile Abate,Gregg, Bertin,John J., Forsythe,James R., Schuricht,Paul H. American Institute of Aeronautics and Astronautics
3 Technical Paper Wind tunnel tests and computational analysis of the CAN1A projectile at Mach 8.2 Edwards, J.A., Roper, J.J., Cleaves, J.A., Dupuis, A.D. American Institute of Aeronautics and Astronautics	9 Technical Paper Supersonic Flowfield for a Slender, Power-Law Elliptic-Section (PLES) Projectile Pesek, Timothy W., Bertin, John J., Forsythe, James R., Pluntze, Stephen C., Schuricht, Paul H., Abate, Greg American Institute of Aeronautics and Astronautics
4 Technical Paper Wind Tunnel Tests of a Grid Finned Projectile Configuration Berner,C., Dupuis,A. American Institute of Aeronautics and Astronautics	10 Technical Paper Analysis of free-flight data for the CAN4 hypersonic research projectile Dupuis, A., Edwards, J.A. American Institute of Aeronautics and Astronautics
5 Technical Paper An Overview of the CAN4 Research Projectile Programme Edwards, J A, Roper, J J, Dupuis, A D, Fournier, E Y American Institute of Aeronautics and Astronautics	11 Technical Paper Return to Flight Testing of a 3.5% Scale Space Shuttle OTS and OT Model at Mach Numbers of 3.5 and 4.0 T. Wadhams, M. MacLean, M. Holden, G. Smolinski American Institute of Aeronautics and Astronautics
6 Technical Paper CALIBRATION OF THE DERA HSST MACH 5 NOZZLE WITH CENTRE BODY Edwards, J.A., Orchard, D.M. American Institute of Aeronautics and Astronautics	12 Conference Proceedings A High Power Enhancement- Mode Pseudomorphic High Electron Mobility Transistor With 2.5w Output Power and 64.5% Efficiency at 3V Chen, S.H., Chang, E.Y., Lin, Y.C. SPIE-The International Society for Optical Engineering

1

2

3

4

5

6

7

8

9

10

11

12