Experimental and analytical comparison of aerodynamic characteristics of a forward-control missile-Reference-Cited by-同舟云学术

Experimental and analytical comparison of aerodynamic characteristics of a forward-control missile

Published:1980-01-14 Issue: Volume: Page:
ISSN:
Container-title:18th Aerospace Sciences Meeting
language:
Short-container-title:

Author:

BLAIR A.¹,RAPP G.²

Affiliation:

1. NASA, Langley Research Center, High-Speed AerodynamicsDiv., Hampton, Va.

2. Motorola, Inc., Government Electronics Div., Scottsdale, Ariz.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1980-374

Reference8 articles.

1. Nielren. Jack N.HemsCh,MichaelJ. and Smith. Charles A.'Preliminary Method tor Calculating the Aerodynamic Characteristic$ of Cruciform Missiles to High AnglesofAttmU IncludingEffectsofRoliAngleandControlDeflections.Otficeot Naval Research Report ONR-CR215-226-4F.1 November 1977.

2. Dilleniur. Marnix F.E. and Nielsen, Jack N.Computer Programs for Calculsting PressureDislribUtionS IncludingVonexEffectsonSuperonicMonoplaneorcru-Cilorm Wing-Body-Tail Combinations with Roundor EliiptiCai Bodies. NEARTR 154,August 1978.

3. Rodman. R.W,Supersonic NormalForceandCenterof PrOLreCharBCteriStiC of LowAspect RatioTrapezoidal Wings.HughesAircraftCompany Memo 224t-t/ 531.4 May 1964.

Cited by 3 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Experimental study of tail-span effects on a canard-controlled missile;Journal of Spacecraft and Rockets;1993-09

2. Evaluation of missile aerodynamic characteristics using rapid prediction techniques;Journal of Spacecraft and Rockets;1984-11

3. Comparison of Analytical and Experimental Supersonic Aerodynamic Characteristics of a Forward Control Missile;Journal of Spacecraft and Rockets;1982-03