Upload
others
View
6
Download
0
Embed Size (px)
Citation preview
DISTRIBUTION: 1p.
2801 Mercer
2801 Koeppel
2801 Kariya
2801 Taylor
2801 Goodman
2801 Byrd
2801 Marks
2801 OSD Technicians
TRANSONIC TUNNEL 1-1
U.S. Army Aviation & Missile Command - LCPK Missile
16-FOOT TT TEST 516
TUNNEL ENTRY DATE: March 22, 1999
TUNNEL EXIT DATE: April 9. 1999
Approval: (SignatureIDate
Lead Test Engineer:
NATIONAL AERONAUTICS AND SPACE ADMINISTRATION LANGLEY RESEARCH CENTER
1.2 Test Meeting Schedule Meeting Name First Meeting Initial Test Planning Meeting Preliminary Test Plan Review Model Design Reviews Final Test Plan Review Pre-test Meeting Staff Briefing Test Readiness Review In-Test Review End-of Test Staff Debriefing
1 . General Test Information ~ 7 -
1.1 Test Personnel
1.1.1 16-Foot Test Team
Meeting Time hiformal Informal 1/26/99 Informal Informal 2/24/99 Informal 3/22/99 Informal 4/9/99
Name Wes Goodman
Jim Byrd
Lloyd Marks Tim Kariya Andrew B oney Charles Mercer Mike Taylor Gary Koeppel
Meeting # M1 M2 R1 R2 R3 M3 M4 R4 R5 M5
RoleRitle Test Project Engineer
Alt.TestProjectEngineer
Test DirectorIAlt. T.P.E. Data Specialist .
Data Specialist Facility Manager Facility Coordinator Instrumentation Coordinator
1.1.2 Research Team NIA
1.1.3 Other Support Personnel
Telephone (W) 45725 (H) 244-5527 (W)45961 (H) 874-3 104 X43066 X43037 X43034 X43043 X459 13 X44835
ip-
E-mail w.l.goodman@larc
j.e.byrd@larc
1.r.marks @larc t.t.kariya@larc a.d.boney @ l a c c.e.mercer@larc r.m.taylor@larc g.e.koeppel@larc
MIS 280
280
280 280 280 280 280 280
Name Roger Cundiff Greg Humphreys Mark Motter John Casadevall William Salyer (Sal) Jack Hughes Ray Rhew ETTD Cellular
Telephone X47848 X46980 X46978 865-0000 (289) X43526 X44110 X44705 879-5578
RoleRitle Automation control engineer Automation control engineer Automation control engineer Modcomp DAS programmer Photographer supervisor NDE supervisor Balance coordinator Instrumentation
E-mail r.l.cundiff @larc g.l.humphreys@larc m.a.motter@larc NIA w.c.salyer@larc j.t.hughes@larc r.d.rhew @larc
MIS 442 442 442 NIA 425 397 238
1 . 4 Test Documentation Required ?r 1.4.1 Customer Requirements Form
1.4.2 Test Plan
1.4.3 Model Request Form
1.4.4 Model Safety Report
1.4.5 16-Foot TT Request for Support
1.4.6 Model Installation Form
1.4.7 Post-test Debriefing
1.4.8 Post-test Data Transmittal Letter '
2 . Test Program
2.1 Test Description
2.1 .1 General Test Description 6 Force and Moment test for the MRDEC configuration (LCPK).
Force and Moment test with user provided instrumentation for special data measurements for the Tracor configuration.
2.1.2 Specific Test Objectives Data to select the proper' canard design Confirm pitch, yaw & roll control with spinning tails Build up data to evaluate canard downwash effect on tails Confirm superposition approach for aerodynamic modeling Identify proper aerodynamic variables for documentary test in June Evaluate potential for sting-model grounding in documentary test in June Confirm the functionality and durability of the spinning tail section
anard roll control valuate requirement for spinning tail Canard selection Determine optimum canard span
anard location xamine stability and contr Nose shapes Evaluate drag of alternative nose shapes
uate aerodynamic modeling of co controls at arbitrary roll angles
Out-of-plane forces Evaluate yawing moment due to roll control canarddownwash Evaluate effect on free spinning vs. locked
tail
Fixed strakes on nose Tailoring missile stability
3 . Model < 3 .1 Model Description
Stinger
3.1.1 Brief Model Description Long slender missiles with canard controls and spinning tail sections.
T.S. T.S. T.S. T.S. T.S.
3.1.2 General Model Geometnr orcelmoment (stability and
1559.0
M.S. 72.0
, 11 392 2 5 608 -
1635.0
M.S. 1.0
_I 2 00,
1600.0
. 35 00 -
3.1 .3 Model ConfiguratiodGeometric Variables Three basic models; Marconi (TRACOR) Two spinning tail sections; locked or free to spin.
LCPK
Model Total lengthk67.5
Remotely operated canards. LCPK Spinning tail section; locked or free to spin.
1647.0
- 3 1 15 - - 25 10 - Aft Pos~tion
u 1 n
scale:FULL ' I
1 1, 72, & 1 Body Diaj2.75 in I
Three nose shapes. Two sets of canards with settings for Pitch, Yaw, & Roll. Two placements for the canards Stinger Spinning tail section; locked or free to spin. Three nose shapes.
1 703.28
U UI
Macon1
675 11
Two sets of canards.
3.1.4 Special Model Requirements/Characteristics Fluid filled tubes for high speed pressure readings. Remotely movable canards on TRACOR model.
3.1 .5 Model Surface Geometry Definition NI A
Transition Location and Type Description